EP3612440A1 - Adjustable joint assembly - Google Patents

Adjustable joint assembly

Info

Publication number
EP3612440A1
EP3612440A1 EP18721704.7A EP18721704A EP3612440A1 EP 3612440 A1 EP3612440 A1 EP 3612440A1 EP 18721704 A EP18721704 A EP 18721704A EP 3612440 A1 EP3612440 A1 EP 3612440A1
Authority
EP
European Patent Office
Prior art keywords
housing
shaft
joint assembly
assembly
diameter portion
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP18721704.7A
Other languages
German (de)
French (fr)
Other versions
EP3612440B1 (en
Inventor
Edward MASON
Florian Itta
Mark Famy
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Saint Gobain Performance Plastics Rencol Ltd
Original Assignee
Saint Gobain Performance Plastics Rencol Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Saint Gobain Performance Plastics Rencol Ltd filed Critical Saint Gobain Performance Plastics Rencol Ltd
Publication of EP3612440A1 publication Critical patent/EP3612440A1/en
Application granted granted Critical
Publication of EP3612440B1 publication Critical patent/EP3612440B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C25/00Bearings for exclusively rotary movement adjustable for wear or play
    • F16C25/02Sliding-contact bearings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62KCYCLES; CYCLE FRAMES; CYCLE STEERING DEVICES; RIDER-OPERATED TERMINAL CONTROLS SPECIALLY ADAPTED FOR CYCLES; CYCLE AXLE SUSPENSIONS; CYCLE SIDE-CARS, FORECARS, OR THE LIKE
    • B62K19/00Cycle frames
    • B62K19/18Joints between frame members
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62KCYCLES; CYCLE FRAMES; CYCLE STEERING DEVICES; RIDER-OPERATED TERMINAL CONTROLS SPECIALLY ADAPTED FOR CYCLES; CYCLE AXLE SUSPENSIONS; CYCLE SIDE-CARS, FORECARS, OR THE LIKE
    • B62K25/00Axle suspensions
    • B62K25/04Axle suspensions for mounting axles resiliently on cycle frame or fork
    • B62K25/12Axle suspensions for mounting axles resiliently on cycle frame or fork with rocking arm pivoted on each fork leg
    • B62K25/22Axle suspensions for mounting axles resiliently on cycle frame or fork with rocking arm pivoted on each fork leg with more than one arm on each fork leg
    • B62K25/26Axle suspensions for mounting axles resiliently on cycle frame or fork with rocking arm pivoted on each fork leg with more than one arm on each fork leg for rear wheel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C17/00Sliding-contact bearings for exclusively rotary movement
    • F16C17/10Sliding-contact bearings for exclusively rotary movement for both radial and axial load
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2226/00Joining parts; Fastening; Assembling or mounting parts
    • F16C2226/10Force connections, e.g. clamping
    • F16C2226/16Force connections, e.g. clamping by wedge action, e.g. by tapered or conical parts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00Articles relating to transporting
    • F16C2326/20Land vehicles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00Articles relating to transporting
    • F16C2326/20Land vehicles
    • F16C2326/26Bicycle steering or suspension

Definitions

  • This disclosure relates to an apparatus comprising matin inner and outer components, where one of the inner or outer component is able to rotate relative to the other.
  • the apparatus can be used for a rotary joint assembly.
  • a joint assembly can be used to adjust, enhance, or limit the amount of torque being transferred from an inner component (such as a shaft), to an outer component (such as housing).
  • a joint assembly can be used in a variety of applications including vehicle frames and bicycle frames to adjust the relative position of one segment or component relative to another.
  • bicycle frames may include rotary joints which use ball bearings. This may create packaging and weight issues.
  • Some bicycle frames use plain bearing rotary joints, but this leads to looseness (radial and axial free-play) which affects the tolerance related performance of the frame. Further problems can occur joint assemblies and rotary joints due to overload situations, larger size and complexity of assembly, varying torque over a lifetime due to wear or abrasion of the components of the assembly, or performance of the joint assembly components being dependent on temperature or other conditions.
  • FIG. 1 is perspective view of a joint assembly according to an embodiment of the invention
  • FIG. 2 is a side view of a joint assembly within an assembly or subassembly according to an embodiment of the invention
  • FIG. 3 is a cross-sectional view of a joint assembly according to an
  • FIG. 4 is a cut-away unassembled side view of a joint assembly according to an embodiment of the invention.
  • FIG. 5 is a cut-away unassembled end view of a joint assembly according to an embodiment of the invention
  • FIG. 6A is a cross-sectional view of a spring element according to an embodiment of the invention.
  • FIG. 6B is a perspective view of a spring element according to an embodiment of the invention.
  • a joint assembly 2 generally includes an inner component and an outer component directed along a central axis 100 that axially down the cross-section of the joint assembly.
  • the inner component may be in the form of a shaft 4 having a first end 4a and a second end 4b.
  • a torque supplying input or torque receiving output can be operatively connected to or engaged with the shaft 4.
  • the shaft 4 may be a single solid component piece, in an embodiment the shaft 4 may include subcomponents including, but not limited to, a first shaft 5 and a second shaft 7.
  • the first shaft 5 may have a first axial end 5a and a second axial end 5b along the axial length of the first shaft 5.
  • the second shaft 7 may have a first axial end 7a and a second axial end 7b along the axial length of the second shaft 7.
  • the shaft 4 may have an inner diameter portion 101 and an outer diameter portion 103.
  • the shaft 4 may have a tapered surface 4'.
  • the tapered surface 4' may have a first axial end 4'a and a second axial end 4'b.
  • the tapered surface 4' may be on at least one of the inner diameter portion 101 or the outer diameter portion 103 of the shaft 4.
  • the first shaft 5 may have a tapered surface 5 ⁇ and/or the second shaft 7 may have a tapered surface 7'.
  • the tapered surface 5' may have a first axial end 5'a and a second axial end 5'b.
  • the tapered surface T may have a first axial end 7'a and a second axial end 7'b.
  • the tapered surface 5' may be on at least one of the inner diameter portion 101 or the outer diameter portion 103 of the first shaft 5.
  • the tapered surface T may be on at least one of the inner diameter portion 101 or the outer diameter portion 103 o the second shaft 7.
  • first shaft 5 and the second shaft 7 may be substantially identical components that may be interchangeable within the joint assembly 2.
  • at least one of the shaft 4, first shaft 5, or second shaft 7 may include an internal bore 13 from the first axial end 4a, 5a, 7a to the second axial end 4b, 5b, 7b along the axial length.
  • the shaft 4 may be made of a material conventional in the art such as, but not limited to, a metal or metal alloy, a polymer, or a composite material.
  • the shaft 4 may be a metal including steel, aluminum, bronze, stainless steel, nickel, copper, tin, titanium, platinum, tungsten, or may be another type.
  • the shaft 4 may include a carbon based compound.
  • the shaft 4 may be manufactured by a method conventional in the art such as, but not limited to, metalworking, forming, forging, extrusion, molding, printing, or may be another type.
  • the outer component may be in the form of a housing 8.
  • the torque receiving input or output can be operatively connected to or engaged with the housing 8.
  • the housing 8 may be a single solid component piece.
  • the housing 8 may include subcomponents including, but not limited to, a first housing 10 and a second housing 12.
  • the first housing 10 may have a first axial end 10a and a second axial end 10b along the axial length of the first housing 10.
  • the second housing 12 may have a first axial end 12a and a second axial end 12b along the axial length of the second housing 12.
  • the housing 8 may have an inner diameter portion 105 and an outer diameter portion 107.
  • the housing 8 may have a tapered surface 8'.
  • the tapered surface 8' may have a first axial end 8'a and a second axial end 8 * b.
  • the tapered surface 10' may have a first axial end 10'a and a second axial end 10'b.
  • the tapered surface 12' may have a first axial end 12'a and a second axial end 12'b.
  • the tapered surface 8' may be on at least one of the inner diameter portion 105 or the outer diameter portion 107 of the housing 8.
  • the first housing may have a tapered surface 10'
  • the second housing 12 may have a tapered surface 12'.
  • the tapered surface 10' may be on at least one of the inner diameter portion 105 or the outer diameter portion 107 of the first housing 10.
  • the tapered surface 12 ' may be on at least one of the inner diameter portion 105 or the outer diameter portion 107 of the second housing 12.
  • the first housing 10 and the second housing 12 may be substantially identical components that may be interchangeable within the joint assembly 2.
  • at least one of the housing 8, first housing 10, or second housing 12 may include an internal bore 16 from the first axial end 8a, 10a, 12a to the second axial end 8b, 10b, 12b along the axial length.
  • the housing 8 may be made of a material conventional in the art such as, but not limited to, a metal or metal alloy, a polymer, or a composite material.
  • the housing 8 may be a metal including steel, aluminum, bronze, stainless steel, nickel, copper, tin, titanium, platinum, tungsten, or may be another type.
  • the housing 8 may include a carbon based compound.
  • the housing 8 may be manufactured by a method conventional in the art such as, but not limited to, metalworking, forming, forging, extrusion, molding, printing, or may be another type.
  • the torque supplying input and the torque receiving output may be operatively coupled together.
  • the torque supplying input can be coupled to a torque generating device (not illustrated) while the torque receiving output may be coupled to a machine requiring torque (not illustrated).
  • the torque receiving output may be in the form of or operatively connected to a shaft 4, and the torque supplying input may be in the form of or operatively connected to a housing 8.
  • the torque receiving output may be in the form of or operatively connected to a housing 8, and the torque supplying input may be in the form of or operatively connected to a shaft 4.
  • the shaft 4 can be receivable into the bore 16 formed in the housing 8.
  • the shaft 4 and the housing 8 can at least partially mate with each other through insertion of the shaft 4 into the bore 16.
  • the outer diameter portion 103 of the shaft 4 may be complementary in shape to the inner diameter portion 105 of the housing 8.
  • the inner diameter portion 101 of the shaft 4 may be complementary in shape to the outer diameter portion 107 of the housing 8.
  • the tapered surface 4' of the shaft 4 be complementary in shape to the tapered surface 8 of the housing 8'.
  • the tapered surface 5' of the first shaft 5 may be complementary in shape to the tapered surface 10' of the first housing 10'.
  • the tapered surface T of the second shaft 7 may be complementary in shape to the tapered surface 12' of the second housing 12'.
  • the tapered surface 4 * of the outer diameter portion 103 of the shaft 4 be complementary in shape to the tapered surface 8' of the inner diameter portion 105 of the housing 8.
  • the tapered surface 5' of the outer diameter portion 103 of the first shaft 5 may be complementary in shape to the tapered surface 10' of the inner diameter portion 105 of the first housing 10'.
  • the tapered surface 7' of the outer diameter portion 103 of the second shaft 7 may be complementary in shape to the tapered surface 12' of the inner diameter portion 105 of the second housing 12'.
  • the tapered surface 4' of the inner diameter portion 101 of the shaft 4 be complementary in shape to the tapered surface 8' of the outer diameter portion 107 of the housing 8.
  • the tapered surface 5' of the inner diameter portion 101 of the first shaft 5 may be complementary in shape to the tapered surface 10' of the outer diameter portion 107 of the first housing 10'.
  • the tapered surface T of inner diameter portion 101 of the second shaft 7 may be complementary in shape to the tapered surface 12' of the outer diameter portion 107 of the second housing 12'.
  • the shaft 4 may rotate relative to the housing 8 within the joint assembly 2.
  • the housing 8 may rotate relative to the shaft 4 within the joint assembly 2.
  • At least one o the tapered surface 4' of the shaft 4, tapered surface 5' of the first shaft 5, or the tapered surface T of the second shaft 7 may be sloped in the axial direction along it exterior surface.
  • the tapered surface 4' of the shaft 4, tapered surface 5' of the first shaft 5, or the tapered surface 7' of the second shaft 7 may be sloped in the axial direction to form an angle a with respect to a line parallel to the central axis 100.
  • the angle a may be between ⁇ a ⁇ 89 ° , such 5 ° ⁇ a ⁇ 45 ° , such as 5° ⁇ a ⁇ 30 ° , such as 10° ⁇ a ⁇ 30 ° .
  • At least one of the tapered surface 8' of the shaft 8, tapered surface 10' of the first housing 10, or the tapered surface 12 " of the second housing 12 may be sloped in the axial direction along it exterior surface.
  • the tapered surface 8' of the shaft 8, tapered surface 10' of the first housing 10, or the tapered surface 12' of the second housing 12 may be sloped in the axial direction to form an angle a with respect to a line parallel to the central axis 100.
  • the angle a may be between ⁇ a ⁇ 89 ° , such 5" ⁇ a ⁇ 45", such as 5 ° ⁇ a ⁇ 30 ' , such as 10 ° ⁇ a ⁇ 30 ° .
  • an axial end 4a of the shaft 4 may include a flared edge 1 14.
  • a cross-section of the flared edge 1 14 may include a circular, polygonal, rounded, oval, or modified rounded shape.
  • an axial end 8a of the housing 8 (or any of its subcomponents) may include a flared edge 1 16.
  • a cross-section of the flared edge 1 16 may include a circular, polygonal, rounded, oval, or modified rounded shape.
  • the tapered surface 4' of the shaft 4 or the tapered surface 8' of the housing 8 may be adapted to adjust or modify torque or frictional fit between the shaft 4 and the housing 8 (or any of their respective subcomponents) by modifying the axial position between the between the shaft 4 and the housing 8 to modify or set a torque value for the joint assembly 2.
  • the polymer layer 20 can be frictionally coupled to at least one of the shaft 4 or the housing 8 (or any of their respective subcomponents). That is, engagement between the polymer layer 20 and one of the shaft 4 or the housing 8 (or any of their respective subcomponents) can occur through frictional resistance.
  • the tapered surface 4' of the shaft 4 (or any of its
  • the radial step 22 may rigidly or fixedly couple the shaft 4 to the housing 8.
  • the tapered surface 8' of the housing 8 (or any of its subcomponents) may include a radial step 24 formed on the inner diameter portion 105.
  • the radial step 24 may rigidly or fixedly couple the shaft 4 to the housing 8.
  • the joint assembly 2 may further include a polymer layer 20.
  • the polymer layer 20 may be coupled to the inner diameter portion 105 of the housing 8 (or any of its respective subcomponents).
  • the polymer layer 20 may be coupled to the outer diameter portion 101 of the shaft 4 (or any of its respective subcomponents).
  • the polymer layer 20 may be provided between the shaft 4 and the housing 8.
  • the polymer layer 20 may be provided on a tapered surface 4' of the shaft 4.
  • the polymer layer 20 may be provided on at least one of the tapered surface 5' of the first shaft 5 or the tapered surface 7' of the second shaft 7.
  • the polymer layer 20 may be provided on a tapered surface 8' of the housing 8.
  • the polymer layer 20 may be provided on at least one of the tapered surface 10' of the first housing 10 or the tapered surface 12' of the second housing 12.
  • a first polymer layer 20a may be provided between the first shaft 5 and the housing 10.
  • a second polymer layer 20b may be provided between the second shaft 7 and the second housing 12.
  • the polymer layer 20 may have a thickness Tp of at least .05 mm, at least .10 mm, at least .15 mm, at least .20 mm, at least .30 mm, at least .40 mm.
  • the polymer layer 20 may have a thickness Tp may be no greater than .5 mm, no greater than .10 mm, no greater than .15 mm, no greater than .20 mm, no greater than .30 mm, no greater than .40 mm.
  • the thickness Tp may vary along the axial length Lp.
  • the polymer layer 20 can have an axial length, Lp, as measured between axial ends 21 , 23 of no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm.
  • the polymer layer 20 can have an axial length, Lp, as measured between axial ends 21 , 23 of at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm.
  • the thickness Tp may vary along the axial length Lp.
  • the polymer layer 20 adapted to adjust or modify torque or frictional fit between the shaft 4 and the housing 8 (or any of their respective subcomponents) by modifying the axial position between the between the shaft 4 and the housing 8 (or any of their respective subcomponents) to modify or set a torque value for the joint assembly 2.
  • the polymer layer 20 can be frictionally coupled to at least one of the shaft 4 or the housing 8 (or any of their respective subcomponents). That is, engagement between the polymer layer 20 and one of the shaft 4 or the housing 8 (or any of their respective subcomponents) can occur through frictional resistance. In this way, a frictional fit may be provided between one of the shaft 4 or the housing 8 (or any of their respective subcomponents).
  • the polymer layer 20 may be provided in the form of a bearing 200 where the bearing 200 includes a substrate 210 and the secondary polymer layer 220 provided on the substrate 210.
  • the substrate 210 can include a metal, for non-limiting example, aluminum, steel, bronze, copper or alloys thereof.
  • the polymer layer 20 or secondary polymer layer 220 may include a polyketone, a polyaramid, a polyimide, a
  • the polymer layer 20 or secondary polymer layer 220 may include a fluoropolymer.
  • the polymer layer 20 or secondary polymer layer 220 may include polytetrafluoroethylene (PTFE), modified polytetrafluoroethylene (mPTFE), ethylene-tetrafluoroethy!ene (ETFE), perfluoroalkoxyethylene (PFA), tetrafluoroethyiene-hexafluoropropylene (FEP), tetrafluoro-ethylene-perf!uoro (methyl vinyl ether) (MFA), polyvinyl idene fluoride (PVDF), ethyl ene- chlorotrifluoroethylene (ECTFE), polyimide (PI), polyamidimide (PAI),
  • PTFE polytetrafluoroethylene
  • mPTFE modified polytetrafluoroethylene
  • ETFE ethylene-tetrafluoroethy!ene
  • PFA perfluoroalkoxyethylene
  • FEP tetrafluoroethyiene-hexafluoro
  • polyphenylene sulfide PPS
  • polyethersulofone PES
  • polyphenylene sulfone PPS02
  • liquid crystal polymers LCP
  • polyetherketone PE
  • polyether ether ketones PEEK
  • aromatic polyesters Ekonol
  • PEEK polyether-ether-ketone
  • PEK polyetherketone
  • LCP polyamide
  • PA polyamide
  • polyoxymethylene POM
  • PE polyethylene
  • PP polypropylene
  • polystyrene polystyrene butadiene copolymers
  • polyesters polycarbonate
  • polyacrylonitriles polyamides, styrenic block copolymers, ethylene vinyl alcohol copolymers, ethylene vinyl acetate copolymers, polyesters grafted with maleic anhydride, poly-vinylidene chloride, aliphatic polyketone, liquid crystalline polymers, ethylene methyl acrylate copolymer, ethyl ene-norbomene copolymers,
  • the polymer layer 20 can be provided to fit the shaft 4 and the housing 8 8 (or any of their respective subcomponents) together to provide a frictional fit between the shaft 4 or the housing 8 (or any of their respective subcomponents).
  • the polymer layer 20 or secondary polymer layer 220 can include one or more fillers such as graphite, glass, aromatic polyester
  • the polymer layer 20 or secondary polymer layer 220 include both graphite and polyester fillers. Concentrations of each of these fillers in a polymer such as PTFE may be greater than 1 %, greater than 5%, greater than 10%, greater than 20% or greater than 25% by weight. Additional layers, such as a bronze mesh between the metal and the fluoropolymer, or embedded in the fluoropolymer, can also be used. Examples o such materials can include the NORGLIDE ® line of products available from Saint-Gobain Performance Plastics Inc. Suitable examples of
  • NORGLIDE products include NORGLIDE PRO, M, SM, T and SMTL.
  • the shaft 4, first shaft 5, or second shaft 7 may have an inner radius Rsi of at least 2.5 mm, at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm.
  • the inner radius Rsi may be no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm.
  • the shaft 4, first shaft 5, or second shaft 7 may have an outer radius Rsi of at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm.
  • the outer radius Rs 2 may be no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm.
  • the shaft 4, first shaft 5, or second shaft 7 can have an axial length, Ls, as measured between axial ends (4a, 4b for shaft 4; 5a, 5b for first shaft 5; 7a, 7b for second shaft) of no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm.
  • the shaft 4, first shaft 5, or second shaft 7 can have an axial length, Ls, as measured between axial ends (4a, 4b for shaft 4; 5a, 5b for first shaft 5; 7a, 7b for second shaft) of at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm.
  • the inner radius Rsi may vary along the axial length Ls.
  • the outer radius Rs 2 may vary along the axial length Ls.
  • the housing 8, first housing 10, or second housing 12 may have an inner radius RH I of at least 2.5mm, at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm.
  • the inner radius RHI may be no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm.
  • the housing 8, first housing 10, or second housing 12 may have an outer radius R H 2 of at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm.
  • the outer radius RH2 may be no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm.
  • the housing 8, first housing 10, or second housing 12 can have an axial length, Ln, as measured between axial ends (8a, 8b for housing 8; 10a, 10b for first housing 10; 12a, 12b for second housing 12) of no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm.
  • the housing 8, first housing 10, or second housing 12 can have an axial length, L 3 ⁇ 4 as measured between axial ends (8a, 8b for housing 8; 10a, 10b for first housing 10; 12a, 12b for second housing 12) of at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm.
  • the inner radius RHI may vary along the axial length Ls.
  • the outer radius R H 2 may vary along the axial length Ls.
  • the joint assembly 2 can include a connecting component 50.
  • the connecting component 50 may have a first axial end 51 and a second axial end 53 along the axial length.
  • the connecting component 50 may connect the first shaft 5 to the second shaft 7.
  • the connecting component 5 may connect the first housing 10 to the second housing 12.
  • the connecting component 50 may include screw threads or other form of threads, bolts, battens, buckle, clamp, clip, flange, frog, grommet, hook- and-eye, latch, peg, nail, rivet, screw anchor, snap fastener, stitch, threaded fastener, tie, toggle bolt, wedge anchor, hole and screw combination, or may be coupled a different way.
  • the inner diameter portion 101 or outer diameter portion 103 of at least one of the first shaft 5 or the second shaft 7 may couple to the connecting component 50 through screw threads or other form of threads, bolts, battens, buckle, clamp, clip, flange, frog, grommet, hook-and-eye, latch, peg, nail, rivet, screw anchor, snap fastener, stitch, threaded fastener, tie, toggle bolt, wedge anchor, hole and screw combination, or may be coupled a different way.
  • the inner diameter portion 105 or outer diameter portion 107 of at least one of the first housing 10 or the second housing 12 may couple to the connecting component 50 through screw threads or other form of threads, bolts, battens, buckle, clamp, clip, flange, frog, grommet, hook-and-eye, latch, peg, nail, rivet, screw anchor, snap fastener, stitch, threaded fastener, tie, toggle bolt, wedge anchor, hole and screw combination, or may be coupled a diff erent way.
  • screw threads of the connecting component 50 may couple to screw threads on the inner diameter portion 101 of the first shaft 5 and the second shaft 7 through the bore 13.
  • screw threads of the connecting component 50 may couple to screw threads on the outer diameter portion 103 of the first shaft 5 and the second shaft 7. In an embodiment , screw threads of the connecting component 50 may couple to screw threads on the inner diameter portion 105 of the first housing 10 and the second housing 12 through the bore 16. In an embodiment, screw threads of the connecting component 50 may couple to screw threads on the outer diameter portion 107 of the first housing 10 and the second housing 12. In a number of embodiments, the connecting component 50 may extend through each of the first shaft 5 and the second shaft 7 and be adapted to provide a biasing force to fix the axial position of the first shaft 5 and the second shaft 8 relative to the first housing 10 and the second housing 12 respectively. In an embodiment, the connecting component 50 may include a threaded screw having a head portion 52 and a thread portion 54.
  • the connecting component 50 may have a radius Rc of at least 1.5 mm, at least 2.5 mm, at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm.
  • the radius Rc may be no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm.
  • the connecting component 50 may can have an axial length, Lc, as measured between axial ends 51 , 53 of no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm.
  • the connecting component 50 may can have an axial length, Lc, as measured between axial ends 51 , 53 of at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm.
  • the radius Rc may vary along the axial length Lc.
  • the joint assembly 2 can include at least one cap component 60.
  • the cap component 60 may have a first axial end 61 a and a second axial end 61 b along the axial length.
  • the cap component 60 may have an internal bore 67 from the first axial end 61 a to the second axial end 61 b along the axial length.
  • the internal bore 67 may be threaded at a first axial end 61 a to pair with another component (not shown).
  • the internal bore 67 may have a polygonal or non-round cross-section to pair with another component (not shown).
  • the cap component 60 may cap the first shaft 5 or the second shaft 7. In an embodiment, the cap component 60 may cap the first housing 10 or the second housing 12.
  • the cap component 60 may include screw threads or other form of threads, bolts, battens, buckle, clamp, clip, flange, frog, grommet, hook-and-eye, latch, peg, nail, rivet, screw anchor, snap fastener, stitch, threaded fastener, tie, toggle bolt, wedge anchor, hole and screw combination, or may be coupled a different way.
  • the inner diameter portion 101 or outer diameter portion 103 of at least one of the first shaft 5 or the second shaft 7 may couple to the cap component 60 through screw threads or other form of threads, bolts, battens, buckle, clamp, clip, flange, frog, grommet, hook-and-eye, latch, peg, nail, rivet, screw anchor, snap fastener, stitch, threaded fastener, tie, toggle bolt, wedge anchor, hole and screw- combination, or may be coupled a different way.
  • the inner diameter portion 105 or outer diameter portion 107 of at least one of the first housing 10 or the second housing 12 may couple to the cap component 60 through screw threads or other form of threads, bolts, battens, buckle, clamp, clip, flange, frog, grommet, hook-and-eye, latch, peg, nail, rivet, screw anchor, snap fastener, stitch, threaded fastener, tie, toggle bolt, wedge anchor, hole and screw combination, or may be coupled a different way.
  • screw threads of the cap component 60 may couple to screw threads on the inner diameter portion 101 of the first shaft 5 and the second shaft 7.
  • screw threads of the cap component 60 may couple to screw threads on the outer diameter portion 103 of the first shaft 5 and the second shaft 7. In an embodiment, screw threads o the cap component 60 may couple to screw threads on the inner diameter portion 105 of the first housing 10 and the second housing 12. In an embodiment, screw threads of the cap component 60 may couple to screw threads on the outer diameter portion 107 of the first housing 10 and the second housing 12. In a number of embodiments, the cap component 60 may cap an axial end 4a, 4b o the shaft 4 (or at least one of the first shaft 5 or the second shaft 7).
  • the cap component 60 may cap an axial end 8a, 8b of the housing 8 (or at least one of the first housing 10 or the second housing 12).
  • the cap component 60 may include a threaded screw having a head portion 62 and a thread portion 64.
  • a first cap component 60a may couple to an outer bore 80a of the bore 13 in the first shaft 5.
  • the first cap component 60a may be coupled to the first shaft 5 through matching screw threads 133.
  • a second cap component 60b may couple to an outer bore 80b of the bore 13 in the second shaft 7.
  • the second cap component 60b may be coupled to the second shaft 7 through matching screw threads 135.
  • the cap component 60 may have a radius Rcc of at least 2.5 mm, at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm.
  • the radius Rcc may be no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm.
  • the cap component 60 may can have an axial length, Lcc, as measured between axial ends 51 , 53 of no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm.
  • the cap component 60 may can have an axial length, Lcc, as measured between axial ends 51 , 53 of at least 5 mm, at least 10 mm, at least 15 mm. at least 20 mm, at least 30 mm, at least 40 mm.
  • the radius Rcc may vary along the axial length Lcc
  • the tapered portion 4' of the shaft 4 may for an interface 300 with the tapered portion 8' of the shaft 8 (or any of its subcomponents 10' 12').
  • the first axial end 4'a of the tapered portion 4' of the shaft 4 may form an outer interface 300a with the first axial end 8 " a of the tapered portion 8' of the housing 8 (or any of its subcomponents 1 l 'a, 12'a).
  • the second axial end 4'b of the tapered portion 4' of the shaft 4 (or any of its
  • subcomponents 5'b, 7'b) may form an inner interface 300b with the second axial end 8'b of the tapered portion 8' of the housing 8 (or any of its subcomponents 1 1 'b, 12'b).
  • at least one of the interface 300, outer interface 300a, or inner interface 300b may be sealed.
  • at least one of the interface 300, outer interface 300a, or inner interface 300b may be sealed by an annular seal.
  • at least one of the interface 300, outer interface 300a, or inner interface 300b may be sealed by an annular seal along the substantial circumference of the interface 300, 300a, 300b.
  • the torque assembly 2 may include a lubricant on any of its components.
  • the lubricant may include a grease including at least one of lithium soap, lithium disulfide, graphite, mineral or vegetable oil, silicone grease, fluorether- based grease, apiezon, food-grade grease, petrochemical grease, or may be a different type.
  • the lubricant may include an oil including at least one of a Group I-GroupIII+ oil, paraffinic oil, naphthenic oil, aromatic oil, biolubricant, castor oil, canola oil, palm oil, sunflower seed oil, rapeseed oil, tall oil, lanolin, synthetic oil, polyalpha- olefin, synthetic ester, polyalkylene glycol, phosphate ester, alkylated naphthalene, silicate ester, ionic fluid, multiply alkylated cyclopentane, petrochemical based, or may be a different type.
  • a Group I-GroupIII+ oil paraffinic oil, naphthenic oil, aromatic oil, biolubricant, castor oil, canola oil, palm oil, sunflower seed oil, rapeseed oil, tall oil, lanolin, synthetic oil, polyalpha- olefin, synthetic ester, polyalkylene glycol, phosphate ester, alkylated naphthalene, silicate
  • the lubricant may include a solid based lubricant including at least one of lithium soap, graphite, boron nitride, molybdenum disulfide, tungsten disulfide, polytetrafluoroethylene, a metal, a metal alloy, or may be a different type.
  • the joint assembly 2 may further include at least one spring element 202.
  • the spring element 202 may be provided between the shaft 4 (or any of its subcomponents), and the housing 8 (and any of its subcomponents).
  • the spring element 202 may be located between the connecting component 50 and the first shaft 5 or second shaft 7.
  • the spring element 202 may compensate for a drop in torque over the life of the joint assembly 2 between the first or second shafts 5, 7, and the connecting component 50. Further, the spring element 202 may be located between the connecting component 50 and the cap assembly 60a, 60b.
  • the spring element 202 may compensate for a drop in torque over the life of the joint assembly 2 between the cap assembly 60a, 60b and the connecting component 50.
  • the spring element 202 may have a compound layer 212 thereon.
  • the spring element 202 may be adapted to modify torque between the shaft 4 (or any of its subcomponents), and the housing 8 (and any of its subcomponents).
  • the spring element 202 may be adapted to provide a biasing force such that the shaft 4 (or any of its subcomponents) may be biased against the housing 8 (and any of its subcomponents).
  • the spring element 202 may have a spring force of at least 0.
  • the spring element 202 may have a spring rate of at least about 1 N/ram. about 10 N/mm, about 25 N/mm, about 50 N/mm, about 100 N/mm, about 200 N/mm, about 500 N/mm, about 1000 N/mm, about 2000 N/mm, about 5000 N/mm, about 10000 N/mm.
  • the at least one spring element 202 can include a first spring element 202A and a first spring element 202 B.
  • the spring element 202 may include a spring element 202 bore 206.
  • At least one of the spring element 202 may have a radius RSE of at least 0.5 mm, of at least 2 mm, of at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm.
  • the radius RSE that may be no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm.
  • the spring element 202 may have an axial thickness TSE, of at least 0.5 mm, of at least 1 mm, of at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm.
  • the axial thickness TS E may be no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm.
  • the radius R SE may vary along the axial length TSE.
  • spring element 202 may include a compound layer 208 thereon.
  • the compound layer 208 can include two or more layers on an exterior surface 205 of the spring element 202.
  • the compound layer 208 can include a first layer 229 and a second layer 231.
  • the compound layer 208 can include at least one polymer.
  • Exemplary polymers can include polytetrafluoroethylene (PTFE), fluorinated ethylene-propylene (FEP), polyvinylidenfluoride (PVDF), polychlorotrifluoroethylene (PCTFE), ethylene chlorotri fluoroethylene (ECTFE), perfluoroalkoxy alkane (PFA), polyacetal, polybutylene terephthalate (PBT), polyethylene terephthalate (PET), polyimide (PI), polyetherimide, polyetheretherketone (PEEK), polyethylene (PE), polysulfone, polyamide (PA), polyphenylene oxide, polyphenylene sulfide (PPS), polyurethane, polyester, liquid crystal polymers (LCP), or any combination thereof.
  • the compound layer 22 can include two or more polymers.
  • the compound layer 208 further includes at least one filler.
  • the filler can enhance the slip interface of the compound layer 208.
  • Exemplary fillers include glass fibers, carbon libers, silicon, PEEK, aromatic polyester, carbon particles, bronze, fluoropolymers, thermoplastic fillers, aluminum oxide,
  • PAI polyamidimide
  • PPS polyphenylene sulfone
  • LCP aromatic polyesters
  • molybdenum disulfide molybdenum disulfide
  • tungsten disulfide graphite, grapheme, expanded graphite, boron nitrade, talc, calcium fluoride, or any combination thereof.
  • the filler can include alumina, silica, titanium dioxide, calcium fluoride, boron nitride, mica, Wollastonite, silicon carbide, silicon nitride, zirconia, carbon black, pigments, or any combination thereof.
  • the compound layer 208 may be coupled to a backing layer (not illustrated), or substrate, or be on the surface of the spring element 202 (or any of its subcomponents 202A, 202B), to enhance rigidity and structural support.
  • the compound layer 208 can be applied to the backing layer by a coating technique, such as for example, physical or vapor deposition, spraying, plating, powder coating, or through other chemical or electrochemical techniques.
  • the compound layer 208 can be sintered to the backing layer.
  • the compound layer 208 may be applied by a roll-to-roll coating process, including for example, extrusion coating.
  • the compound layer 208 can be heated to a molten or semi-molten state and extruded through a slot die onto a major surface of the backing layer.
  • the compound layer 208 can be cast or molded.
  • the compound layer 208 can be pressed or rolled to the backing layer. In a particular embodiment, pressing or rolling can occur at elevated temperatures, i.e., the compound layer 208 may be hot- pressed or rolled.
  • an adhesive layer (not illustrated) can be disposed between the compound layer 208 and the backing layer.
  • the joint assembly 2 may include a locking mechanism 70.
  • the locking mechanism 70 may lock the housing 8 (or any of its subcomponents) in place with respect to the shaft 4(or any of its subcomponents).
  • the locking mechanism 70 may include a pin, groove and stop, nut and bolt, nut and screw, latch, handle, locking nut, tie rivet, or may be locked another way.
  • the locking mechanism 70 may include a radial step 22, 24 to lock the joint assembly 2.
  • a radial step 24, 22 may rigidly or fixedly couple the shaft 4 to the housing 8.
  • the joint assembly 2 may be a component within a vehicle subassembly 800.
  • the vehicle subassembly 800 may include a frame 802.
  • the frame may include a plurality of segments 804, 804' as subcomponents.
  • the frame 802 may include a bore 850.
  • the bore 850 may be located at an intersection of two segments 804.
  • the joint assembly 2 may be positioned within the bore 850.
  • the joint assembly 2 may be placed within the bore 850 to control, restrict, or allow relative movement between two adjacent segments 804 based on the axial position and frictional fit of the shaft 4 relative to the housing 8 within the joint assembly 2.
  • the joint assembly 2 may rotate relative to the frame 802.
  • the joint assembly 2, T, 2", 2"', 2"" may be a component within a bicycle assembly 900.
  • the bicycle assembly 900 may include a frame 902.
  • the frame 902 may include a main structure 904 and a support structure 906 as subcomponents.
  • the main structure 904 may include a main triangle 908.
  • the support structure 906 may include a paired rear triangle 910.
  • the main structure 904 or main triangle 908 may include a wheel assembly 912.
  • the support structure 906 or paired rear triangle 910 may include a wheel assembly 912.
  • the wheel assembly 912 may include an axle 914 and a wheel 916.
  • the frame 902 may include a bore 950.
  • the joint assembly 2 may be placed within the bore 950 to control, restrict, or allow relative movement between the main structure 906 and the support structure 906 based on the axial position and frictional fit of the shaft 4 relative to the housing 8 within the joint assembly 2.
  • the joint assembly 2 may be placed within the bore 950 to control, restrict, or allow relative movement between the main triangle 908 and the paired rear triangle 910 based on the axial position and frictional fit of the shaft 4 relative to the housing 8 within the joint assembly 2.
  • the joint assembly 2 may rotate relative to the frame 902.
  • the shaft 4 may be placed within the bore 16 formed in the housing 8.
  • the first shaft 5 may be placed within the bore 16 formed in the first housing 10.
  • the second shaft 7 may be placed within the bore 16 formed in the second housing 12.
  • the connecting component 50 may pair the first shaft 5 with the second shaft 7.
  • the connecting component 50 may pair the first shaft 5 with the second shaft 7 through threadings (or other means) within the bores 13 o the first shaft 5 and the second shaft 7.
  • the connecting component 50 may be used to adjust the axial position of the first shaft 5 relative to the second shaft 7.
  • the connecting component 50 may be used to adjust the axial position of the first housing 10 relative to the second housing 12.
  • the torque provided from the joint assembly 2 can be adjusted to its desired torque level or torque value based on the desired application of the joint assembly 2.
  • tightening, loosening, or otherwise engaging of the connecting component 50 to axially move the first shaft 5 (and first housing 10) and the second shaft 7 (and second housing 12) closer together may alter the transmittable torque between the first shaft 5 (and first housing 10) and the second shaft 7 (and second housing 12) to a desired torque level or value within the joint assembly 2.
  • tightening, loosening, or otherwise engaging of the connecting component 50 to axially move the first housing 10 and the second housing 12 closer together may alter the transmittable torque between the first housing 10 and the second housing 12 to a desired torque level or value within the joint assembly 2 based on the desired application.
  • the to: que level or value may be set constant by no further rotation of the connecting component 50 moving the axial position of the first shaft 5 (and first housing 10) and the second shaft 7 (and second housing 12).
  • the connecting component 50 may be manually tightened to a required torque level or value.
  • the axial spacing of the shaft 4 (or any of its subcomponents) relative to the housing 8 (or any of its subcomponents) may modify or adjust the torque value between the components of the joint assembly 2. In an embodiment, the axial spacing of the shaft 4 (or any of its subcomponents) relative to the housing 8 (or any of its subcomponents) may modify or adjust the frictional fit between the components of the joint assembly 2.
  • the housing 8 may be adapted to have an adjustable torque value or frictional fit to the shaft 4 through the pairing of the tapered surfaces of the shaft 4' coupled to the housing 8'.
  • the first housing 10 may have an adjustable torque value or frictional fit to the first shaft 5 through the pairing of the tapered surfaces of the first shaft 5' coupled to the first housing 10'.
  • the second housing 12 may have an adjustable torque value or frictional fit to the second shaft 7 through the pairing of the tapered surfaces of the second shaft T coupled to the second housing 12'.
  • the polymer layer 20 may provide the frictional fit between the shaft 4 (or any of its subcomponents) and the housing 8 (or any of its subcomponents).
  • this frictional fit may provide a seal between the shaft 4 (or any of its subcomponents) and the housing 8 (or any of its subcomponents). This seal may keep abrasive particles out of the joint assembly 2 (or any of its subcomponents). This seal may keep lubricant from leaking out of the joint assembly 2 (or any of its subcomponents).
  • the frictional fit may be set to a relative constant between the first shaft 5 and the first housing 10 through a locking at the step 22 of the first shaft 7 with the first housing 10.
  • the frictional fit may be set to a relative constant between the second shaft 7 and the second housing 12 through a locking at the step 24 of the second shaft 7 with the second housing 12.
  • the pairing of tapered surfaces of the shaft 4 (or any of its subcomponents) relative to the housing 8 (or any of its subcomponents) may modify or adjust the torque value between the components of the joint assembly 2.
  • the pairing of tapered surfaces of the shaft 4 (or any of its subcomponents) relative to the housing 8 (or any of its subcomponents) may modify or adjust the frietional fit between the components of the joint assembly 2.
  • the cap component 60 may be coupled to the shaft 4 through the bore 13 in the shaft 4. In an embodiment, threadings in the cap component 60 may couple to matching treads in the bore 13 of the shaft. In an embodiment, a cap component 60 may be coupled to the first shaft 5 while a second cap component 60' may be coupled to the second shaft 7.
  • the joint assembly 2 may be assembled or installed within a bore 850 in the frame 802 of a vehicle subassembly 800. In an embodiment, the joint assembly 2 may be assembled or installed within a bore 950 in the frame 902 of a bicycle assembly 900.
  • the joint assembly 2 can be installed or assembled by an assembly force of at least 1 kgf in a longitudinal direction relative to the shaft 4 or housing 8, such as at least 2 kgf, at least 3 kgf, at least 4 kgf, at least 5 kgf, at least 10 kgf, or even at least 15 kgf.
  • the torque assembly 2 can be installed or assembled by an assembly force of no greater than 20 kg in a longitudinal direction to the housing 8, such as no greater than 19 kgf, no greater than 1 8 kgf, no greater than 17 kgf or even no greater than 16 kgf.
  • the provided joint assembly 2 may enable rotary joints to have smaller packaging, increased stiffness, and simplified service within an application while maintaining low friction, sealing, and durability of the joint assembly 2, frame 802, 902, or any subcomponents o either.
  • the joint assembly may provide longer life of the frame 802, 902, easier fit, be noise free, and provide space and weight savings within the bicycle assembly 900 or vehicle subassembly 800.
  • Embodiment 1 A joint assembly comprising: a housing comprising an inner diameter portion having a tapered surface; and at least one shaft having an outer diameter portion having a tapered surface that is complementary in shape to the inner diameter portion of the housing, wherein at least one of the shaft or the housing is adapted to rotate relative to the other, and wherein the factional fit is adjustable by modifying the axial position of the shaft relative to the housing.
  • Embodiment 2 A bicycle assembly comprising: a bicycle frame comprising: a main structure and a support structure comprising a wheel assembly; and a joint assembly located within the bicycle frame adapted to modify the position of the wheel assembly to the main assembly, the joint assembly comprising: a housing comprising an inner diameter portion having a tapered surface; and at least one shaft having an outer diameter portion having a tapered surface that is complementary in shape to the inner diameter portion of the housing, wherein at least one of the shaft or the housing is adapted to rotate relative to the other, and wherein the frictional fit is adjustable by modifying the axial position of the shaft relative to the housing.
  • Embodiment 3 A vehicle subassembly comprising: a frame; and a component rotatably attached to the frame by a joint assembly located within the frame, the joint assembly comprising: a housing comprising an inner diameter portion having a tapered surface; and at least one shaft having an outer diameter portion having a tapered surface that is complementary in shape to the inner diameter portion of the housing, wherein at least one of the shaft or the housing is adapted to rotate relative to the other, and wherein the frictional fit is adjustable by modifying the axial position of the shaft relative to the housing.
  • Embodiment 4 A method comprising: providing a jointed apparatus comprising a frame having a bore; fitting a joint assembly within the bore of the frame, the joint assembly comprising: a housing comprising an inner diameter portion having a tapered surface; and at least one shaft having an outer diameter portion having a tapered surface that is complementary in shape to the inner diameter portion of the housing, wherein at least one of the shaft or the housing is adapted to rotate relative to the other; and adjusting a position of the shaft within the housing to provide a frictional fit between the housing and the shaft.
  • Embodiment 5 The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any one of the preceding embodiments, further comprising a polymer layer between the shaft and the housing.
  • Embodiment 6 The joint assembly, bicycle frame assembly, vehicle subassembly, or method of embodiment 5, wherein the polymer layer comprises a fiuorinated polymer.
  • Embodiment 7 The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 5-6, wherein the polymer layer is coupled to the inner diameter portion of the housing.
  • Embodiment 8 The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 5-7, wherein the polymer layer is coupled to the outer diameter portion of the shaft.
  • Embodiment 9 The joint assembly, bicycle frame assembly, vehicle subassembly, or method o any of embodiments 5-8, wherein the polymer layer is provided in the form of a bearing, the bearing including a substrate on which the polymer layer is provided.
  • Embodiment 10 The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any one of embodiments 1 to 9, further comprising a step formed in the tapered surface of the shaft or tapered surface of the housing to prevent axial movement of the bearing.
  • Embodiment 1 1 The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 -10, wherein the at least one housing comprises a first housing and a second housing.
  • Embodiment 12 The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 -1 1 , wherein the at least one shaft comprises a first shaft and a second shaft.
  • Embodiment 13 The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 - 12, wherein the shaft comprises a connecting component connecting the first shaft to the second shaft.
  • Embodiment 14 The joint assembly, bicycle frame assembly, vehicle subassembly, or method of embodiment 13, wherein the connecting component extends through each of the first and second shafts and is adapted to provide a biasing force to fix the axial position of the first and second shafts relative to the first and second housings respectively.
  • Embodiment 15 The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 -14, wherein the tapered surface of the inner diameter portion of the at least one housing has an angle a relative to an axis of the housing, , wherein ⁇ a ⁇ 89 ' , such 5 ° ⁇ a ⁇ 45 ⁇ such as 5 ° ⁇ a ⁇ 30°, such as 10° ⁇ ⁇ ⁇ 30 ' .
  • Embodiment 16 The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 -15, wherein the tapered surface of the outer diameter of the at least one shaft has an angle a relative to an axis of the housing, wherein 1 ' ⁇ a ⁇ 89°, such 5° ⁇ a ⁇ 45 ° , such as 5 ° ⁇ a ⁇ 30 ° , such as 10° ⁇ a ⁇ 30 ° .
  • Embodiment 17 The joint assembly, bicycle frame assembly, vehicle subassembly, or method f any of embodiments 1 -16, wherein the shaft comprises a metal.
  • Embodiment 18 The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 - 17, wherein the housing comprises a metal.
  • Embodiment 19 The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1-18, wherein the at least one of the housing or at least one shaft further comprises a lubricant disposed at an interface between housing and shaft.
  • Embodiment 20 The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 -19, wherein the tapered portion of the shaft has an inner end and an outer end, the housing has an inner end and outer end, and at least one of an outer interface between the tapered portion of the shaft and the housing at the outer end or an inner interface between the tapered portion of the shaft and the housing at the inner end, wherein at least one of an outer or inner interface is sealed.
  • Embodiment 21 The joint assembly, bicycle frame assembly, vehicle subassembly, or method of embodiment 20, wherein the outer interface or inner interface between the shaft and the housing is sealed with an annular seal.
  • Embodiment 22 The bicycle frame assembly of embodiments 2 and 5-21 , wherein the joint assembly is provided as a rocker pivot, main pivot, chain stay pivot, or pull leverage pivot of the bicycle frame assembly.
  • Embodiment 23 The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 -22, wherein the shaft can be readjusted within the housing to provide a frictional fit and axial force between the housing and the shaft.
  • Embodiment 24 The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 -23, further comprising at least one spring element to provide a biasing force such that the shaft is biased against the housing.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Sliding-Contact Bearings (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
  • Motorcycle And Bicycle Frame (AREA)
  • Gasket Seals (AREA)

Abstract

A joint assembly including a housing including an inner diameter portion having a tapered surface; and at least one shaft having an outer diameter portion having a tapered surface that is complementary in shape to the inner diameter portion of the housing, where the shaft is adapted to rotate relative to the housing, and where the frictional fit is adjustable by modifying the axial position of the shaft relative to the housing.

Description

ADJUSTABLE JOINT ASSEMBLY
TECHNICAL FIELD
This disclosure relates to an apparatus comprising matin inner and outer components, where one of the inner or outer component is able to rotate relative to the other. By non-limiting example, the apparatus can be used for a rotary joint assembly.
A joint assembly can be used to adjust, enhance, or limit the amount of torque being transferred from an inner component (such as a shaft), to an outer component (such as housing). A joint assembly can be used in a variety of applications including vehicle frames and bicycle frames to adjust the relative position of one segment or component relative to another. Commonly, bicycle frames may include rotary joints which use ball bearings. This may create packaging and weight issues. Some bicycle frames use plain bearing rotary joints, but this leads to looseness (radial and axial free-play) which affects the tolerance related performance of the frame. Further problems can occur joint assemblies and rotary joints due to overload situations, larger size and complexity of assembly, varying torque over a lifetime due to wear or abrasion of the components of the assembly, or performance of the joint assembly components being dependent on temperature or other conditions.
BRIEF DESCRIPTION OF THE DRAWINGS
The present disclosure may be better understood, and its numerous features and advantages made apparent to those skilled in the art by referencing the accompanying drawings.
FIG. 1 is perspective view of a joint assembly according to an embodiment of the invention;
FIG. 2 is a side view of a joint assembly within an assembly or subassembly according to an embodiment of the invention;
FIG. 3 is a cross-sectional view of a joint assembly according to an
embodiment of the invention;
FIG. 4 is a cut-away unassembled side view of a joint assembly according to an embodiment of the invention;
FIG. 5 is a cut-away unassembled end view of a joint assembly according to an embodiment of the invention; FIG. 6A is a cross-sectional view of a spring element according to an embodiment of the invention; and
FIG. 6B is a perspective view of a spring element according to an embodiment of the invention.
The use of the same reference symbols in different drawings indicates similar or identical items.
DETAILED DESCRIPTIO OF THE PREFERRED EMBODIMENT(S)
The following description in combination with the figures is provided to assist in understanding the teachings disclosed herein. The following discussion will focus on specific implementations and embodiments of the teachings. This focus is provided to assist in describing the teachings and should not be interpreted as a limitation on the scope or applicability of the teachings. However, other
embodiments can be used based on the teachings as disclosed in this application.
The terms '"comprises," "comprising," "includes," "including," "has,"
"having" or any other variation thereof, are intended to cover a non-exclusive inclusion. For example, a method, article, or apparatus that comprises a list of features is not necessarily limited only to those features but may include other features not expressly listed or inherent to such method, article, or apparatus. Further, unless expressly stated to the contrary, "or" refers to an inclusive-or and not to an exclusive-or. For example, a condition A or B is satisfied by any one of the following: A is true (or present) and B is false (or not present), A is false (or not present) and B is true (or present), and both A and B are true (or present).
Also, the use of "a" or "an" is employed to describe elements and components described herein. This is done merely for convenience and to give a general sense of the scope of the invention. This description should be read to include one, at least one, or the singular as also including the plural, or vice versa, unless it is clear that it is meant otherwise. For example, when a single item is described herein, more than one item may be used in place o a single item. Similarly, where more than one item is described herein, a single item may be substituted for that more than one item. Also, the use of "about" or "substantially" is employed to convey spatial or numerical relationships that describe any value or relationship that does not depart from the scope of the invention. Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The materials, methods, and examples are illustrative only and not intended to be limiting. To the extent not described herein, many details regarding specific materials and processing acts are conventional and may be found in textbooks and other sources within the joint assembly and torque adjustable component arts.
Referring initially to FIGS. 1 and 3-5, a joint assembly 2 generally includes an inner component and an outer component directed along a central axis 100 that axially down the cross-section of the joint assembly. In an embodiment, the inner component may be in the form of a shaft 4 having a first end 4a and a second end 4b. In another embodiment, a torque supplying input or torque receiving output can be operatively connected to or engaged with the shaft 4. The shaft 4 may be a single solid component piece, in an embodiment the shaft 4 may include subcomponents including, but not limited to, a first shaft 5 and a second shaft 7. The first shaft 5 may have a first axial end 5a and a second axial end 5b along the axial length of the first shaft 5. The second shaft 7 may have a first axial end 7a and a second axial end 7b along the axial length of the second shaft 7. In an embodiment the shaft 4 may have an inner diameter portion 101 and an outer diameter portion 103. The shaft 4 may have a tapered surface 4'. The tapered surface 4' may have a first axial end 4'a and a second axial end 4'b. The tapered surface 4' may be on at least one of the inner diameter portion 101 or the outer diameter portion 103 of the shaft 4. In an embodiment the first shaft 5 may have a tapered surface 5\ and/or the second shaft 7 may have a tapered surface 7'. The tapered surface 5' may have a first axial end 5'a and a second axial end 5'b. The tapered surface T may have a first axial end 7'a and a second axial end 7'b. In an embodiment the tapered surface 5' may be on at least one of the inner diameter portion 101 or the outer diameter portion 103 of the first shaft 5. In an embodiment the tapered surface T may be on at least one of the inner diameter portion 101 or the outer diameter portion 103 o the second shaft 7. In an
embodiment, the first shaft 5 and the second shaft 7 may be substantially identical components that may be interchangeable within the joint assembly 2. In an embodiment, at least one of the shaft 4, first shaft 5, or second shaft 7 may include an internal bore 13 from the first axial end 4a, 5a, 7a to the second axial end 4b, 5b, 7b along the axial length.
In an embodiment, the shaft 4 may be made of a material conventional in the art such as, but not limited to, a metal or metal alloy, a polymer, or a composite material. The shaft 4 may be a metal including steel, aluminum, bronze, stainless steel, nickel, copper, tin, titanium, platinum, tungsten, or may be another type. The shaft 4 may include a carbon based compound. In an embodiment, the shaft 4 may be manufactured by a method conventional in the art such as, but not limited to, metalworking, forming, forging, extrusion, molding, printing, or may be another type.
In an embodiment, the outer component may be in the form of a housing 8. In another embodiment, the torque receiving input or output can be operatively connected to or engaged with the housing 8. The housing 8 may be a single solid component piece. In an embodiment the housing 8 may include subcomponents including, but not limited to, a first housing 10 and a second housing 12. The first housing 10 may have a first axial end 10a and a second axial end 10b along the axial length of the first housing 10. The second housing 12 may have a first axial end 12a and a second axial end 12b along the axial length of the second housing 12. In an embodiment the housing 8 may have an inner diameter portion 105 and an outer diameter portion 107. The housing 8 may have a tapered surface 8'. The tapered surface 8' may have a first axial end 8'a and a second axial end 8*b. The tapered surface 10' may have a first axial end 10'a and a second axial end 10'b. The tapered surface 12' may have a first axial end 12'a and a second axial end 12'b. The tapered surface 8' may be on at least one of the inner diameter portion 105 or the outer diameter portion 107 of the housing 8. In an embodiment, the first housing may have a tapered surface 10', and/or the second housing 12 may have a tapered surface 12'. In an embodiment, the tapered surface 10' may be on at least one of the inner diameter portion 105 or the outer diameter portion 107 of the first housing 10. In an embodiment the tapered surface 12' may be on at least one of the inner diameter portion 105 or the outer diameter portion 107 of the second housing 12. In a number of variations, the first housing 10 and the second housing 12 may be substantially identical components that may be interchangeable within the joint assembly 2. In an embodiment, at least one of the housing 8, first housing 10, or second housing 12 may include an internal bore 16 from the first axial end 8a, 10a, 12a to the second axial end 8b, 10b, 12b along the axial length.
In an embodiment, the housing 8 may be made of a material conventional in the art such as, but not limited to, a metal or metal alloy, a polymer, or a composite material. The housing 8 may be a metal including steel, aluminum, bronze, stainless steel, nickel, copper, tin, titanium, platinum, tungsten, or may be another type. The housing 8 may include a carbon based compound. In an embodiment, the housing 8 may be manufactured by a method conventional in the art such as, but not limited to, metalworking, forming, forging, extrusion, molding, printing, or may be another type.
In an embodiment, the torque supplying input and the torque receiving output may be operatively coupled together. The torque supplying input can be coupled to a torque generating device (not illustrated) while the torque receiving output may be coupled to a machine requiring torque (not illustrated). In an embodiment, the torque receiving output may be in the form of or operatively connected to a shaft 4, and the torque supplying input may be in the form of or operatively connected to a housing 8. In another embodiment, the torque receiving output may be in the form of or operatively connected to a housing 8, and the torque supplying input may be in the form of or operatively connected to a shaft 4.
Still referring to FIGs. 1 and 3-5, in an embodiment, the shaft 4 can be receivable into the bore 16 formed in the housing 8. The shaft 4 and the housing 8 can at least partially mate with each other through insertion of the shaft 4 into the bore 16. In an embodiment, the outer diameter portion 103 of the shaft 4 may be complementary in shape to the inner diameter portion 105 of the housing 8. In an embodiment, the inner diameter portion 101 of the shaft 4 may be complementary in shape to the outer diameter portion 107 of the housing 8. In an embodiment, the tapered surface 4' of the shaft 4 be complementary in shape to the tapered surface 8 of the housing 8'. In an embodiment, the tapered surface 5' of the first shaft 5 may be complementary in shape to the tapered surface 10' of the first housing 10'. In an embodiment, the tapered surface T of the second shaft 7 may be complementary in shape to the tapered surface 12' of the second housing 12'.
In an embodiment, the tapered surface 4* of the outer diameter portion 103 of the shaft 4 be complementary in shape to the tapered surface 8' of the inner diameter portion 105 of the housing 8. In an embodiment, the tapered surface 5' of the outer diameter portion 103 of the first shaft 5 may be complementary in shape to the tapered surface 10' of the inner diameter portion 105 of the first housing 10'. In an embodiment, the tapered surface 7' of the outer diameter portion 103 of the second shaft 7 may be complementary in shape to the tapered surface 12' of the inner diameter portion 105 of the second housing 12'. In an embodiment, the tapered surface 4' of the inner diameter portion 101 of the shaft 4 be complementary in shape to the tapered surface 8' of the outer diameter portion 107 of the housing 8. In an embodiment, the tapered surface 5' of the inner diameter portion 101 of the first shaft 5 may be complementary in shape to the tapered surface 10' of the outer diameter portion 107 of the first housing 10'. In an embodiment, the tapered surface T of inner diameter portion 101 of the second shaft 7 may be complementary in shape to the tapered surface 12' of the outer diameter portion 107 of the second housing 12'. In a number of embodiments, the shaft 4 may rotate relative to the housing 8 within the joint assembly 2. In a number of embodiments, the housing 8 may rotate relative to the shaft 4 within the joint assembly 2.
In an embodiment, at least one o the tapered surface 4' of the shaft 4, tapered surface 5' of the first shaft 5, or the tapered surface T of the second shaft 7 may be sloped in the axial direction along it exterior surface. The tapered surface 4' of the shaft 4, tapered surface 5' of the first shaft 5, or the tapered surface 7' of the second shaft 7 may be sloped in the axial direction to form an angle a with respect to a line parallel to the central axis 100. The angle a may be between Γ< a < 89°, such 5°< a < 45°, such as 5°< a < 30°, such as 10°< a < 30°. In an embodiment, at least one of the tapered surface 8' of the shaft 8, tapered surface 10' of the first housing 10, or the tapered surface 12" of the second housing 12 may be sloped in the axial direction along it exterior surface. The tapered surface 8' of the shaft 8, tapered surface 10' of the first housing 10, or the tapered surface 12' of the second housing 12 may be sloped in the axial direction to form an angle a with respect to a line parallel to the central axis 100. The angle a may be between Γ< a < 89°, such 5"< a < 45", such as 5°< a < 30 ', such as 10°< a < 30°.
In an embodiment, an axial end 4a of the shaft 4 (or any of its subcomponents) may include a flared edge 1 14. A cross-section of the flared edge 1 14 may include a circular, polygonal, rounded, oval, or modified rounded shape. In an embodiment, an axial end 8a of the housing 8 (or any of its subcomponents) may include a flared edge 1 16. A cross-section of the flared edge 1 16 may include a circular, polygonal, rounded, oval, or modified rounded shape.
In an embodiment, the tapered surface 4' of the shaft 4 or the tapered surface 8' of the housing 8 (or any of their respective subcomponents) may be adapted to adjust or modify torque or frictional fit between the shaft 4 and the housing 8 (or any of their respective subcomponents) by modifying the axial position between the between the shaft 4 and the housing 8 to modify or set a torque value for the joint assembly 2. The polymer layer 20 can be frictionally coupled to at least one of the shaft 4 or the housing 8 (or any of their respective subcomponents). That is, engagement between the polymer layer 20 and one of the shaft 4 or the housing 8 (or any of their respective subcomponents) can occur through frictional resistance. In a number of variations, the tapered surface 4' of the shaft 4 (or any of its
subcomponents) may include a radial step 22 formed on the outer diameter portion 103. In a number of variations, the radial step 22 may rigidly or fixedly couple the shaft 4 to the housing 8. In a number of variations, the tapered surface 8' of the housing 8 (or any of its subcomponents) may include a radial step 24 formed on the inner diameter portion 105. In a number of variations, the radial step 24 may rigidly or fixedly couple the shaft 4 to the housing 8.
Still referring to FIGs. 1 and 3-5, the joint assembly 2 may further include a polymer layer 20. In an embodiment, the polymer layer 20 may be coupled to the inner diameter portion 105 of the housing 8 (or any of its respective subcomponents). In an embodiment, the polymer layer 20 may be coupled to the outer diameter portion 101 of the shaft 4 (or any of its respective subcomponents).The polymer layer 20 may be provided between the shaft 4 and the housing 8. The polymer layer 20 may be provided on a tapered surface 4' of the shaft 4. The polymer layer 20 may be provided on at least one of the tapered surface 5' of the first shaft 5 or the tapered surface 7' of the second shaft 7. The polymer layer 20 may be provided on a tapered surface 8' of the housing 8. The polymer layer 20 may be provided on at least one of the tapered surface 10' of the first housing 10 or the tapered surface 12' of the second housing 12. In an embodiment, a first polymer layer 20a may be provided between the first shaft 5 and the housing 10. In an embodiment, a second polymer layer 20b may be provided between the second shaft 7 and the second housing 12. In an embodiment, the polymer layer 20 may have a thickness Tp of at least .05 mm, at least .10 mm, at least .15 mm, at least .20 mm, at least .30 mm, at least .40 mm. The polymer layer 20 may have a thickness Tp may be no greater than .5 mm, no greater than .10 mm, no greater than .15 mm, no greater than .20 mm, no greater than .30 mm, no greater than .40 mm. The thickness Tp may vary along the axial length Lp. In an embodiment, the polymer layer 20 can have an axial length, Lp, as measured between axial ends 21 , 23 of no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm. The polymer layer 20 can have an axial length, Lp, as measured between axial ends 21 , 23 of at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm. The thickness Tp may vary along the axial length Lp.
In an embodiment, the polymer layer 20 adapted to adjust or modify torque or frictional fit between the shaft 4 and the housing 8 (or any of their respective subcomponents) by modifying the axial position between the between the shaft 4 and the housing 8 (or any of their respective subcomponents) to modify or set a torque value for the joint assembly 2. The polymer layer 20 can be frictionally coupled to at least one of the shaft 4 or the housing 8 (or any of their respective subcomponents). That is, engagement between the polymer layer 20 and one of the shaft 4 or the housing 8 (or any of their respective subcomponents) can occur through frictional resistance. In this way, a frictional fit may be provided between one of the shaft 4 or the housing 8 (or any of their respective subcomponents).
In an embodiment, the polymer layer 20 may be provided in the form of a bearing 200 where the bearing 200 includes a substrate 210 and the secondary polymer layer 220 provided on the substrate 210. In an exemplary embodiment, the substrate 210 can include a metal, for non-limiting example, aluminum, steel, bronze, copper or alloys thereof. In an embodiment, the polymer layer 20 or secondary polymer layer 220 may include a polyketone, a polyaramid, a polyimide, a
polyetherimide, a polyamideimide, a polyphenylene sulfide, a polyphenylene sulfone, a f!uoropolymer, a polybenzimidazole, a derivation thereof, or a combination thereof. In an embodiment, the polymer layer 20 or secondary polymer layer 220 may include a fluoropolymer. In an embodiment, the polymer layer 20 or secondary polymer layer 220 may include polytetrafluoroethylene (PTFE), modified polytetrafluoroethylene (mPTFE), ethylene-tetrafluoroethy!ene (ETFE), perfluoroalkoxyethylene (PFA), tetrafluoroethyiene-hexafluoropropylene (FEP), tetrafluoro-ethylene-perf!uoro (methyl vinyl ether) (MFA), polyvinyl idene fluoride (PVDF), ethyl ene- chlorotrifluoroethylene (ECTFE), polyimide (PI), polyamidimide (PAI),
polyphenylene sulfide (PPS), polyethersulofone (PES), polyphenylene sulfone (PPS02), liquid crystal polymers (LCP), polyetherketone (PE ), polyether ether ketones (PEEK), aromatic polyesters (Ekonol), of polyether-ether-ketone (PEEK), polyetherketone (PEK), liquid crystal polymer (LCP), polyamide (PA),
polyoxymethylene (POM), polyethylene (PE) / UHMPE, polypropylene (PP), polystyrene, styrene butadiene copolymers, polyesters, polycarbonate,
polyacrylonitriles, polyamides, styrenic block copolymers, ethylene vinyl alcohol copolymers, ethylene vinyl acetate copolymers, polyesters grafted with maleic anhydride, poly-vinylidene chloride, aliphatic polyketone, liquid crystalline polymers, ethylene methyl acrylate copolymer, ethyl ene-norbomene copolymers,
polymethylpentene and ethylene acyrilic acid copoloymer, mixtures, copolymers and any combination thereof. In an embodiment, the polymer layer 20 can be provided to fit the shaft 4 and the housing 8 8 (or any of their respective subcomponents) together to provide a frictional fit between the shaft 4 or the housing 8 (or any of their respective subcomponents).
In a particular aspect, the polymer layer 20 or secondary polymer layer 220 can include one or more fillers such as graphite, glass, aromatic polyester
(EKONOL®), bronze, zinc, boron nitride, carbon and/or polyimide. Moreover, in one aspect, the polymer layer 20 or secondary polymer layer 220 include both graphite and polyester fillers. Concentrations of each of these fillers in a polymer such as PTFE may be greater than 1 %, greater than 5%, greater than 10%, greater than 20% or greater than 25% by weight. Additional layers, such as a bronze mesh between the metal and the fluoropolymer, or embedded in the fluoropolymer, can also be used. Examples o such materials can include the NORGLIDE® line of products available from Saint-Gobain Performance Plastics Inc. Suitable examples of
NORGLIDE products include NORGLIDE PRO, M, SM, T and SMTL.
In an embodiment, the shaft 4, first shaft 5, or second shaft 7 may have an inner radius Rsi of at least 2.5 mm, at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm. The inner radius Rsi may be no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm. In an embodiment, the shaft 4, first shaft 5, or second shaft 7 may have an outer radius Rsi of at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm. The outer radius Rs2 may be no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm. In an
embodiment, the shaft 4, first shaft 5, or second shaft 7 can have an axial length, Ls, as measured between axial ends (4a, 4b for shaft 4; 5a, 5b for first shaft 5; 7a, 7b for second shaft) of no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm. The shaft 4, first shaft 5, or second shaft 7 can have an axial length, Ls, as measured between axial ends (4a, 4b for shaft 4; 5a, 5b for first shaft 5; 7a, 7b for second shaft) of at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm. The inner radius Rsi may vary along the axial length Ls. The outer radius Rs2 may vary along the axial length Ls.
In an embodiment, the housing 8, first housing 10, or second housing 12 may have an inner radius RH I of at least 2.5mm, at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm. The inner radius RHI may be no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm. In an embodiment, the housing 8, first housing 10, or second housing 12 may have an outer radius RH2 of at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm. The outer radius RH2 may be no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm. In an embodiment, the housing 8, first housing 10, or second housing 12 can have an axial length, Ln, as measured between axial ends (8a, 8b for housing 8; 10a, 10b for first housing 10; 12a, 12b for second housing 12) of no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm. The housing 8, first housing 10, or second housing 12 can have an axial length, L¾ as measured between axial ends (8a, 8b for housing 8; 10a, 10b for first housing 10; 12a, 12b for second housing 12) of at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm. The inner radius RHI may vary along the axial length Ls. The outer radius RH2 may vary along the axial length Ls. Still referring to FIGs. 1 and 3-5, in an embodiment, the joint assembly 2 can include a connecting component 50. The connecting component 50 may have a first axial end 51 and a second axial end 53 along the axial length. The connecting component 50 may connect the first shaft 5 to the second shaft 7. In an embodiment, the connecting component 5 may connect the first housing 10 to the second housing 12. In an embodiment, the connecting component 50 may include screw threads or other form of threads, bolts, battens, buckle, clamp, clip, flange, frog, grommet, hook- and-eye, latch, peg, nail, rivet, screw anchor, snap fastener, stitch, threaded fastener, tie, toggle bolt, wedge anchor, hole and screw combination, or may be coupled a different way. In an embodiment, the inner diameter portion 101 or outer diameter portion 103 of at least one of the first shaft 5 or the second shaft 7 may couple to the connecting component 50 through screw threads or other form of threads, bolts, battens, buckle, clamp, clip, flange, frog, grommet, hook-and-eye, latch, peg, nail, rivet, screw anchor, snap fastener, stitch, threaded fastener, tie, toggle bolt, wedge anchor, hole and screw combination, or may be coupled a different way. In an embodiment, the inner diameter portion 105 or outer diameter portion 107 of at least one of the first housing 10 or the second housing 12 may couple to the connecting component 50 through screw threads or other form of threads, bolts, battens, buckle, clamp, clip, flange, frog, grommet, hook-and-eye, latch, peg, nail, rivet, screw anchor, snap fastener, stitch, threaded fastener, tie, toggle bolt, wedge anchor, hole and screw combination, or may be coupled a diff erent way. In an embodiment, screw threads of the connecting component 50 may couple to screw threads on the inner diameter portion 101 of the first shaft 5 and the second shaft 7 through the bore 13. In an embodiment, screw threads of the connecting component 50 may couple to screw threads on the outer diameter portion 103 of the first shaft 5 and the second shaft 7. In an embodiment , screw threads of the connecting component 50 may couple to screw threads on the inner diameter portion 105 of the first housing 10 and the second housing 12 through the bore 16. In an embodiment, screw threads of the connecting component 50 may couple to screw threads on the outer diameter portion 107 of the first housing 10 and the second housing 12. In a number of embodiments, the connecting component 50 may extend through each of the first shaft 5 and the second shaft 7 and be adapted to provide a biasing force to fix the axial position of the first shaft 5 and the second shaft 8 relative to the first housing 10 and the second housing 12 respectively. In an embodiment, the connecting component 50 may include a threaded screw having a head portion 52 and a thread portion 54.
In an embodiment, the connecting component 50 may have a radius Rc of at least 1.5 mm, at least 2.5 mm, at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm. The radius Rc may be no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm. In an embodiment, the connecting component 50 may can have an axial length, Lc, as measured between axial ends 51 , 53 of no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm. The connecting component 50 may can have an axial length, Lc, as measured between axial ends 51 , 53 of at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm. The radius Rc may vary along the axial length Lc.
Referring to FIG. 3, in an embodiment, the joint assembly 2 can include at least one cap component 60. The cap component 60 may have a first axial end 61 a and a second axial end 61 b along the axial length. The cap component 60 may have an internal bore 67 from the first axial end 61 a to the second axial end 61 b along the axial length. The internal bore 67 may be threaded at a first axial end 61 a to pair with another component (not shown). The internal bore 67 may have a polygonal or non-round cross-section to pair with another component (not shown). The cap component 60 may cap the first shaft 5 or the second shaft 7. In an embodiment, the cap component 60 may cap the first housing 10 or the second housing 12. In an embodiment, the cap component 60 may include screw threads or other form of threads, bolts, battens, buckle, clamp, clip, flange, frog, grommet, hook-and-eye, latch, peg, nail, rivet, screw anchor, snap fastener, stitch, threaded fastener, tie, toggle bolt, wedge anchor, hole and screw combination, or may be coupled a different way. In an embodiment, the inner diameter portion 101 or outer diameter portion 103 of at least one of the first shaft 5 or the second shaft 7 may couple to the cap component 60 through screw threads or other form of threads, bolts, battens, buckle, clamp, clip, flange, frog, grommet, hook-and-eye, latch, peg, nail, rivet, screw anchor, snap fastener, stitch, threaded fastener, tie, toggle bolt, wedge anchor, hole and screw- combination, or may be coupled a different way. In an embodiment, the inner diameter portion 105 or outer diameter portion 107 of at least one of the first housing 10 or the second housing 12 may couple to the cap component 60 through screw threads or other form of threads, bolts, battens, buckle, clamp, clip, flange, frog, grommet, hook-and-eye, latch, peg, nail, rivet, screw anchor, snap fastener, stitch, threaded fastener, tie, toggle bolt, wedge anchor, hole and screw combination, or may be coupled a different way. In an embodiment, screw threads of the cap component 60 may couple to screw threads on the inner diameter portion 101 of the first shaft 5 and the second shaft 7. In an embodiment, screw threads of the cap component 60 may couple to screw threads on the outer diameter portion 103 of the first shaft 5 and the second shaft 7. In an embodiment, screw threads o the cap component 60 may couple to screw threads on the inner diameter portion 105 of the first housing 10 and the second housing 12. In an embodiment, screw threads of the cap component 60 may couple to screw threads on the outer diameter portion 107 of the first housing 10 and the second housing 12. In a number of embodiments, the cap component 60 may cap an axial end 4a, 4b o the shaft 4 (or at least one of the first shaft 5 or the second shaft 7). In a number of embodiments, the cap component 60 may cap an axial end 8a, 8b of the housing 8 (or at least one of the first housing 10 or the second housing 12). In an embodiment, the cap component 60 may include a threaded screw having a head portion 62 and a thread portion 64. In a number of embodiments, a first cap component 60a may couple to an outer bore 80a of the bore 13 in the first shaft 5. The first cap component 60a may be coupled to the first shaft 5 through matching screw threads 133. In a number of embodiments, a second cap component 60b may couple to an outer bore 80b of the bore 13 in the second shaft 7. The second cap component 60b may be coupled to the second shaft 7 through matching screw threads 135.
In an embodiment, the cap component 60 may have a radius Rcc of at least 2.5 mm, at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm. The radius Rcc may be no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm. In an embodiment, the cap component 60 may can have an axial length, Lcc, as measured between axial ends 51 , 53 of no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm. The cap component 60 may can have an axial length, Lcc, as measured between axial ends 51 , 53 of at least 5 mm, at least 10 mm, at least 15 mm. at least 20 mm, at least 30 mm, at least 40 mm. The radius Rcc may vary along the axial length Lcc
In an embodiment, the tapered portion 4' of the shaft 4 (or any of its subcomponents 5', 7') may for an interface 300 with the tapered portion 8' of the shaft 8 (or any of its subcomponents 10' 12'). In an embodiment, the first axial end 4'a of the tapered portion 4' of the shaft 4 (or any of its subcomponents 5'a, 7'a) may form an outer interface 300a with the first axial end 8"a of the tapered portion 8' of the housing 8 (or any of its subcomponents 1 l 'a, 12'a). In an embodiment, the second axial end 4'b of the tapered portion 4' of the shaft 4 (or any of its
subcomponents 5'b, 7'b) may form an inner interface 300b with the second axial end 8'b of the tapered portion 8' of the housing 8 (or any of its subcomponents 1 1 'b, 12'b). In an embodiment, at least one of the interface 300, outer interface 300a, or inner interface 300b may be sealed. In an embodiment, at least one of the interface 300, outer interface 300a, or inner interface 300b may be sealed by an annular seal. In an embodiment, at least one of the interface 300, outer interface 300a, or inner interface 300b may be sealed by an annular seal along the substantial circumference of the interface 300, 300a, 300b.
In an embodiment, the torque assembly 2 may include a lubricant on any of its components. The lubricant may include a grease including at least one of lithium soap, lithium disulfide, graphite, mineral or vegetable oil, silicone grease, fluorether- based grease, apiezon, food-grade grease, petrochemical grease, or may be a different type. The lubricant may include an oil including at least one of a Group I-GroupIII+ oil, paraffinic oil, naphthenic oil, aromatic oil, biolubricant, castor oil, canola oil, palm oil, sunflower seed oil, rapeseed oil, tall oil, lanolin, synthetic oil, polyalpha- olefin, synthetic ester, polyalkylene glycol, phosphate ester, alkylated naphthalene, silicate ester, ionic fluid, multiply alkylated cyclopentane, petrochemical based, or may be a different type. The lubricant may include a solid based lubricant including at least one of lithium soap, graphite, boron nitride, molybdenum disulfide, tungsten disulfide, polytetrafluoroethylene, a metal, a metal alloy, or may be a different type.
In an embodiment, as shown in FIGs. 4, 5, 6A-6B, the joint assembly 2 may further include at least one spring element 202. The spring element 202 may be provided between the shaft 4 (or any of its subcomponents), and the housing 8 (and any of its subcomponents). In an embodiment, as shown in FIG. 3, the spring element 202 may be located between the connecting component 50 and the first shaft 5 or second shaft 7. The spring element 202 may compensate for a drop in torque over the life of the joint assembly 2 between the first or second shafts 5, 7, and the connecting component 50. Further, the spring element 202 may be located between the connecting component 50 and the cap assembly 60a, 60b. The spring element 202 may compensate for a drop in torque over the life of the joint assembly 2 between the cap assembly 60a, 60b and the connecting component 50. In an embodiment, the spring element 202 may have a compound layer 212 thereon. The spring element 202 may be adapted to modify torque between the shaft 4 (or any of its subcomponents), and the housing 8 (and any of its subcomponents). The spring element 202 may be adapted to provide a biasing force such that the shaft 4 (or any of its subcomponents) may be biased against the housing 8 (and any of its subcomponents). The spring element 202 may have a spring force of at least 0. 1 N, at least 1 N, at least 5 N, at least I O N, at least 1000 N, at least 1000 N, at least 10000 N. The spring element 202 may have a spring rate of at least about 1 N/ram. about 10 N/mm, about 25 N/mm, about 50 N/mm, about 100 N/mm, about 200 N/mm, about 500 N/mm, about 1000 N/mm, about 2000 N/mm, about 5000 N/mm, about 10000 N/mm.
In an embodiment, as shown in FIGs. 4, 5, and 6A-6B, the at least one spring element 202 can include a first spring element 202A and a first spring element 202 B. The spring element 202 may include a spring element 202 bore 206. In an
embodiment, at least one of the spring element 202 (or any of its subcomponents 202A, 202B), may have a radius RSE of at least 0.5 mm, of at least 2 mm, of at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm. The radius RSE that may be no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm. The spring element 202 (or any of its subcomponents 202A, 202B), may have an axial thickness TSE, of at least 0.5 mm, of at least 1 mm, of at least 5 mm, at least 10 mm, at least 15 mm, at least 20 mm, at least 30 mm, at least 40 mm. The axial thickness TSE that may be no greater than 5 mm, no greater than 10 mm, no greater than 15 mm, no greater than 20 mm, no greater than 30 mm, no greater than 40 mm. The radius RSE may vary along the axial length TSE.
In an embodiment, spring element 202 (or any of its subcomponents 202A, 202B), may include a compound layer 208 thereon. The compound layer 208 can include two or more layers on an exterior surface 205 of the spring element 202. The compound layer 208 can include a first layer 229 and a second layer 231. The compound layer 208 can include at least one polymer. Exemplary polymers can include polytetrafluoroethylene (PTFE), fluorinated ethylene-propylene (FEP), polyvinylidenfluoride (PVDF), polychlorotrifluoroethylene (PCTFE), ethylene chlorotri fluoroethylene (ECTFE), perfluoroalkoxy alkane (PFA), polyacetal, polybutylene terephthalate (PBT), polyethylene terephthalate (PET), polyimide (PI), polyetherimide, polyetheretherketone (PEEK), polyethylene (PE), polysulfone, polyamide (PA), polyphenylene oxide, polyphenylene sulfide (PPS), polyurethane, polyester, liquid crystal polymers (LCP), or any combination thereof. The compound layer 22 can include two or more polymers.
In an embodiment, the compound layer 208 further includes at least one filler. The filler can enhance the slip interface of the compound layer 208. Exemplary fillers include glass fibers, carbon libers, silicon, PEEK, aromatic polyester, carbon particles, bronze, fluoropolymers, thermoplastic fillers, aluminum oxide,
polyamidimide (PAI), PPS, polyphenylene sulfone (PPS02), LCP, aromatic polyesters, molybdenum disulfide, tungsten disulfide, graphite, grapheme, expanded graphite, boron nitrade, talc, calcium fluoride, or any combination thereof.
Additionally, the filler can include alumina, silica, titanium dioxide, calcium fluoride, boron nitride, mica, Wollastonite, silicon carbide, silicon nitride, zirconia, carbon black, pigments, or any combination thereof.
In an embodiment, the compound layer 208 may be coupled to a backing layer (not illustrated), or substrate, or be on the surface of the spring element 202 (or any of its subcomponents 202A, 202B), to enhance rigidity and structural support. The compound layer 208 can be applied to the backing layer by a coating technique, such as for example, physical or vapor deposition, spraying, plating, powder coating, or through other chemical or electrochemical techniques. In a certain embodiment, the compound layer 208 can be sintered to the backing layer. In a particular embodiment, the compound layer 208 may be applied by a roll-to-roll coating process, including for example, extrusion coating. The compound layer 208 can be heated to a molten or semi-molten state and extruded through a slot die onto a major surface of the backing layer. In another embodiment, the compound layer 208 can be cast or molded. In an embodiment, the compound layer 208 can be pressed or rolled to the backing layer. In a particular embodiment, pressing or rolling can occur at elevated temperatures, i.e., the compound layer 208 may be hot- pressed or rolled. In some embodiments, an adhesive layer (not illustrated) can be disposed between the compound layer 208 and the backing layer.
Referring back to F IGs. 1 and 3-5, in an embodiment, the joint assembly 2 may include a locking mechanism 70. The locking mechanism 70 may lock the housing 8 (or any of its subcomponents) in place with respect to the shaft 4(or any of its subcomponents). In an embodiment, the locking mechanism 70 may include a pin, groove and stop, nut and bolt, nut and screw, latch, handle, locking nut, tie rivet, or may be locked another way. As shown in FIG. 1 , in at least one embodiment, the locking mechanism 70 may include a radial step 22, 24 to lock the joint assembly 2. In a number of variations, a radial step 24, 22 may rigidly or fixedly couple the shaft 4 to the housing 8.
In an embodiment, as shown in FIG. 3, the joint assembly 2 may be a component within a vehicle subassembly 800. The vehicle subassembly 800 may include a frame 802. The frame may include a plurality of segments 804, 804' as subcomponents. The frame 802 may include a bore 850. In an embodiment, the bore 850 may be located at an intersection of two segments 804. In an embodiment, the joint assembly 2 may be positioned within the bore 850. The joint assembly 2 may be placed within the bore 850 to control, restrict, or allow relative movement between two adjacent segments 804 based on the axial position and frictional fit of the shaft 4 relative to the housing 8 within the joint assembly 2. In a number of embodiments, the joint assembly 2 may rotate relative to the frame 802.
In an embodiment, as shown in FIG. 2, the joint assembly 2, T, 2", 2"', 2"" may be a component within a bicycle assembly 900. The bicycle assembly 900 may include a frame 902. In an embodiment, the frame 902 may include a main structure 904 and a support structure 906 as subcomponents. In an embodiment, the main structure 904 may include a main triangle 908. In an embodiment, the support structure 906 may include a paired rear triangle 910. In a number of embodiments, the main structure 904 or main triangle 908 may include a wheel assembly 912. In a number of embodiments, the support structure 906 or paired rear triangle 910 may include a wheel assembly 912. In an embodiment, the wheel assembly 912 may include an axle 914 and a wheel 916. In a number of embodiments, the frame 902 may include a bore 950. The joint assembly 2 may be placed within the bore 950 to control, restrict, or allow relative movement between the main structure 906 and the support structure 906 based on the axial position and frictional fit of the shaft 4 relative to the housing 8 within the joint assembly 2. In an embodiment, the joint assembly 2 may be placed within the bore 950 to control, restrict, or allow relative movement between the main triangle 908 and the paired rear triangle 910 based on the axial position and frictional fit of the shaft 4 relative to the housing 8 within the joint assembly 2. In a number of embodiments, the joint assembly 2 may rotate relative to the frame 902.
A method of assembling and using the torque assembly 2 is recited. In an embodiment, the shaft 4 may be placed within the bore 16 formed in the housing 8. In an embodiment, the first shaft 5 may be placed within the bore 16 formed in the first housing 10. In an embodiment, the second shaft 7 may be placed within the bore 16 formed in the second housing 12. In an embodiment, the connecting component 50 may pair the first shaft 5 with the second shaft 7. The connecting component 50 may pair the first shaft 5 with the second shaft 7 through threadings (or other means) within the bores 13 o the first shaft 5 and the second shaft 7. In an embodiment, the connecting component 50 may be used to adjust the axial position of the first shaft 5 relative to the second shaft 7. In an embodiment, the connecting component 50 may be used to adjust the axial position of the first housing 10 relative to the second housing 12.
In this way, the torque provided from the joint assembly 2 can be adjusted to its desired torque level or torque value based on the desired application of the joint assembly 2. In an embodiment, tightening, loosening, or otherwise engaging of the connecting component 50 to axially move the first shaft 5 (and first housing 10) and the second shaft 7 (and second housing 12) closer together may alter the transmittable torque between the first shaft 5 (and first housing 10) and the second shaft 7 (and second housing 12) to a desired torque level or value within the joint assembly 2. In an embodiment, tightening, loosening, or otherwise engaging of the connecting component 50 to axially move the first housing 10 and the second housing 12 closer together may alter the transmittable torque between the first housing 10 and the second housing 12 to a desired torque level or value within the joint assembly 2 based on the desired application. The to: que level or value may be set constant by no further rotation of the connecting component 50 moving the axial position of the first shaft 5 (and first housing 10) and the second shaft 7 (and second housing 12). In an embodiment, the connecting component 50 may be manually tightened to a required torque level or value. In an embodiment, the axial spacing of the shaft 4 (or any of its subcomponents) relative to the housing 8 (or any of its subcomponents) may modify or adjust the torque value between the components of the joint assembly 2. In an embodiment, the axial spacing of the shaft 4 (or any of its subcomponents) relative to the housing 8 (or any of its subcomponents) may modify or adjust the frictional fit between the components of the joint assembly 2.
In an embodiment, the housing 8 may be adapted to have an adjustable torque value or frictional fit to the shaft 4 through the pairing of the tapered surfaces of the shaft 4' coupled to the housing 8'. In an embodiment, the first housing 10 may have an adjustable torque value or frictional fit to the first shaft 5 through the pairing of the tapered surfaces of the first shaft 5' coupled to the first housing 10'. In an embodiment, the second housing 12 may have an adjustable torque value or frictional fit to the second shaft 7 through the pairing of the tapered surfaces of the second shaft T coupled to the second housing 12'. In an embodiment, the polymer layer 20 may provide the frictional fit between the shaft 4 (or any of its subcomponents) and the housing 8 (or any of its subcomponents). In an embodiment, this frictional fit may provide a seal between the shaft 4 (or any of its subcomponents) and the housing 8 (or any of its subcomponents). This seal may keep abrasive particles out of the joint assembly 2 (or any of its subcomponents). This seal may keep lubricant from leaking out of the joint assembly 2 (or any of its subcomponents). In an embodiment, the frictional fit may be set to a relative constant between the first shaft 5 and the first housing 10 through a locking at the step 22 of the first shaft 7 with the first housing 10. In an embodiment, the frictional fit may be set to a relative constant between the second shaft 7 and the second housing 12 through a locking at the step 24 of the second shaft 7 with the second housing 12. In an embodiment, the pairing of tapered surfaces of the shaft 4 (or any of its subcomponents) relative to the housing 8 (or any of its subcomponents) may modify or adjust the torque value between the components of the joint assembly 2. In an embodiment, the pairing of tapered surfaces of the shaft 4 (or any of its subcomponents) relative to the housing 8 (or any of its subcomponents) may modify or adjust the frietional fit between the components of the joint assembly 2.
In an embodiment, the cap component 60 may be coupled to the shaft 4 through the bore 13 in the shaft 4. In an embodiment, threadings in the cap component 60 may couple to matching treads in the bore 13 of the shaft. In an embodiment, a cap component 60 may be coupled to the first shaft 5 while a second cap component 60' may be coupled to the second shaft 7. In an embodiment, the joint assembly 2 may be assembled or installed within a bore 850 in the frame 802 of a vehicle subassembly 800. In an embodiment, the joint assembly 2 may be assembled or installed within a bore 950 in the frame 902 of a bicycle assembly 900.
In an embodiment, the joint assembly 2 can be installed or assembled by an assembly force of at least 1 kgf in a longitudinal direction relative to the shaft 4 or housing 8, such as at least 2 kgf, at least 3 kgf, at least 4 kgf, at least 5 kgf, at least 10 kgf, or even at least 15 kgf. In a further embodiment, the torque assembly 2 can be installed or assembled by an assembly force of no greater than 20 kg in a longitudinal direction to the housing 8, such as no greater than 19 kgf, no greater than 1 8 kgf, no greater than 17 kgf or even no greater than 16 kgf.
The provided joint assembly 2 may enable rotary joints to have smaller packaging, increased stiffness, and simplified service within an application while maintaining low friction, sealing, and durability of the joint assembly 2, frame 802, 902, or any subcomponents o either. The joint assembly may provide longer life of the frame 802, 902, easier fit, be noise free, and provide space and weight savings within the bicycle assembly 900 or vehicle subassembly 800.
Many different aspects and embodiments are possible. Some of those aspects and embodiments are described below. After reading this specification, skilled artisans will appreciate that those aspects and embodiments are only illustrative and do not limit the scope of the present in vention. Embodiments may be in accordance with any one or more of the embodiments as listed below.
Embodiment 1 : A joint assembly comprising: a housing comprising an inner diameter portion having a tapered surface; and at least one shaft having an outer diameter portion having a tapered surface that is complementary in shape to the inner diameter portion of the housing, wherein at least one of the shaft or the housing is adapted to rotate relative to the other, and wherein the factional fit is adjustable by modifying the axial position of the shaft relative to the housing.
Embodiment 2: A bicycle assembly comprising: a bicycle frame comprising: a main structure and a support structure comprising a wheel assembly; and a joint assembly located within the bicycle frame adapted to modify the position of the wheel assembly to the main assembly, the joint assembly comprising: a housing comprising an inner diameter portion having a tapered surface; and at least one shaft having an outer diameter portion having a tapered surface that is complementary in shape to the inner diameter portion of the housing, wherein at least one of the shaft or the housing is adapted to rotate relative to the other, and wherein the frictional fit is adjustable by modifying the axial position of the shaft relative to the housing.
Embodiment 3 : A vehicle subassembly comprising: a frame; and a component rotatably attached to the frame by a joint assembly located within the frame, the joint assembly comprising: a housing comprising an inner diameter portion having a tapered surface; and at least one shaft having an outer diameter portion having a tapered surface that is complementary in shape to the inner diameter portion of the housing, wherein at least one of the shaft or the housing is adapted to rotate relative to the other, and wherein the frictional fit is adjustable by modifying the axial position of the shaft relative to the housing.
Embodiment 4: A method comprising: providing a jointed apparatus comprising a frame having a bore; fitting a joint assembly within the bore of the frame, the joint assembly comprising: a housing comprising an inner diameter portion having a tapered surface; and at least one shaft having an outer diameter portion having a tapered surface that is complementary in shape to the inner diameter portion of the housing, wherein at least one of the shaft or the housing is adapted to rotate relative to the other; and adjusting a position of the shaft within the housing to provide a frictional fit between the housing and the shaft.
Embodiment 5: The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any one of the preceding embodiments, further comprising a polymer layer between the shaft and the housing.
Embodiment 6: The joint assembly, bicycle frame assembly, vehicle subassembly, or method of embodiment 5, wherein the polymer layer comprises a fiuorinated polymer. Embodiment 7: The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 5-6, wherein the polymer layer is coupled to the inner diameter portion of the housing.
Embodiment 8: The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 5-7, wherein the polymer layer is coupled to the outer diameter portion of the shaft.
Embodiment 9: The joint assembly, bicycle frame assembly, vehicle subassembly, or method o any of embodiments 5-8, wherein the polymer layer is provided in the form of a bearing, the bearing including a substrate on which the polymer layer is provided.
Embodiment 10: The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any one of embodiments 1 to 9, further comprising a step formed in the tapered surface of the shaft or tapered surface of the housing to prevent axial movement of the bearing.
Embodiment 1 1 : The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 -10, wherein the at least one housing comprises a first housing and a second housing.
Embodiment 12: The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 -1 1 , wherein the at least one shaft comprises a first shaft and a second shaft.
Embodiment 13: The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 - 12, wherein the shaft comprises a connecting component connecting the first shaft to the second shaft.
Embodiment 14: The joint assembly, bicycle frame assembly, vehicle subassembly, or method of embodiment 13, wherein the connecting component extends through each of the first and second shafts and is adapted to provide a biasing force to fix the axial position of the first and second shafts relative to the first and second housings respectively.
Embodiment 15: The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 -14, wherein the tapered surface of the inner diameter portion of the at least one housing has an angle a relative to an axis of the housing, , wherein Γ< a < 89 ', such 5°< a < 45 \ such as 5°< a < 30°, such as 10°< α < 30 '. Embodiment 16: The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 -15, wherein the tapered surface of the outer diameter of the at least one shaft has an angle a relative to an axis of the housing, wherein 1 '< a < 89°, such 5°< a < 45°, such as 5°< a < 30°, such as 10°< a < 30°.
Embodiment 17: The joint assembly, bicycle frame assembly, vehicle subassembly, or method f any of embodiments 1 -16, wherein the shaft comprises a metal.
Embodiment 18: The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 - 17, wherein the housing comprises a metal.
Embodiment 19: The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1-18, wherein the at least one of the housing or at least one shaft further comprises a lubricant disposed at an interface between housing and shaft.
Embodiment 20: The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 -19, wherein the tapered portion of the shaft has an inner end and an outer end, the housing has an inner end and outer end, and at least one of an outer interface between the tapered portion of the shaft and the housing at the outer end or an inner interface between the tapered portion of the shaft and the housing at the inner end, wherein at least one of an outer or inner interface is sealed.
Embodiment 21 : The joint assembly, bicycle frame assembly, vehicle subassembly, or method of embodiment 20, wherein the outer interface or inner interface between the shaft and the housing is sealed with an annular seal.
Embodiment 22: The bicycle frame assembly of embodiments 2 and 5-21 , wherein the joint assembly is provided as a rocker pivot, main pivot, chain stay pivot, or pull leverage pivot of the bicycle frame assembly.
Embodiment 23 : The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 -22, wherein the shaft can be readjusted within the housing to provide a frictional fit and axial force between the housing and the shaft. Embodiment 24: The joint assembly, bicycle frame assembly, vehicle subassembly, or method of any of embodiments 1 -23, further comprising at least one spring element to provide a biasing force such that the shaft is biased against the housing.
Note that not all of the features described above are required, that a portion of a specific feature may not be required, and that one or more features may be provided in addition to those described. Still further, the order in which features are described is not necessarily the order in which the features are installed.
Certain features are, for clarity, described herein in the context of separate embodiments, may also be provided in combination in a single embodiment.
Conversely, various features that are, for brevity, described in the context of a single embodiment, may also be provided separately or in any subcombinations.
Benefits, other advantages, and solutions to problems have been described above with regard to specific embodiments, However, the benefits, advantages, solutions to problems, and any feature(s) that may cause any benefit, advantage, or solution to occur or become more pronounced are not to be construed as a critical, required, or essential feature of any or all the claims.
The specification and illustrations of the embodiments described herein are intended to provide a general understanding of the structure of the v arious
embodiments. The specification and illustrations are not intended to serve as an exhaustive and comprehensive description of all of the elements and features of apparatus and systems that use the structures or methods described herein. Separate embodiments may also be provided in combination in a single embodiment, and conversely, various features that are, for brevity, described in the context of a single embodiment, may also be provided separately or in any subcombination. Further, reference to values stated in ranges includes each and every value within that range, including the end range values referenced. Many other embodiments may be apparent to skilled artisans only after reading this specification. Other embodiments may be used and derived from the disclosure, such that a structural substitution, logical substitution, or any change may be made without departing from the scope of the disclosure. Accordingly, the disclosure is to be regarded as illustrative rather than restrictive.

Claims

WHAT IS CLAIMED IS:
1. A joint assembly comprising:
a housing comprising an inner diameter portion having a tapered surface; and at least one shaft having an outer diameter portion having a tapered surface that is complementary in shape to the inner diameter portion of the housing, wherein at least one of the shaft or the housing is adapted to rotate relative to the other, and wherein the frictional fit is adjustable by modifying the axial position of the shaft relative to the housing.
2. A bicycle assembly comprising:
a bicycle frame comprising: a main structure and a support structure comprising a wheel assembly; and
a joint assembly located within the bicycle frame adapted to modify the position of the wheel assembly to the main assembly, the joint assembly comprising: a housing comprising an inner diameter portion having a tapered surface; and at least one shaft having an outer diameter portion having a tapered surface that is complementary in shape to the inner diameter portion of the housing, wherein at least one of the shaft or the housing is adapted to rotate relative to the other, and wherein the frictional fit is adjustable by modifying the axial position o the shaft relative to the housing.
3. A vehicle subassembly comprising:
a frame; and
a component rotatably attached to the frame by a joint assembly located within the frame, the joint assembly comprising:
a housing comprising an inner diameter portion having a tapered surface; and at least one shaft having an outer diameter portion having a tapered surface that is complementary in shape to the inner diameter portion of the housing, wherein at least one of the shaft or the housing is adapted to rotate relative to the other, and wherein the frictional fit is adjustable by modifying the axial position of the shaft relative to the housing.
4. The joint assembly, bicycle frame assembly, or vehicle subassembly of any one of the preceding claims, further comprising a polymer layer between the shaft and the housing.
5. The joint assembly, bicycle frame assembly, or vehicle subassembly of claim 4, wherein the polymer layer comprises a fluorinated polymer.
6. The joint assembly, bicycle frame assembly, or vehicle subassembly of claim 4 or 5, wherein the polymer layer is coupled to the inner diameter portion of the housing.
7. The joint assembly, bicycle frame assembly, or vehicle subassembly of claim 4 or 5, wherein the polymer layer is coupled to the outer diameter portion of the shaft.
8. The joint assembly, bicycle frame assembly, or v ehicle subassembly of any one of claims 4 to 7, wherein the polymer layer is provided in the form of a bearing, the bearing including a substrate on which the polymer layer is provided.
9. The joint assembly, bicycle frame assembly, or vehicle subassembly o any one of claims 1 to 8, further comprising a step formed in the tapered surface of the shaft or tapered surface of the housing to prevent axial movement of the bearing.
10. The joint assembly, bicycle frame assembly, or vehicle subassembly o any of claims 1 to 9, wherein the at least one housing comprises a first housing and a second housing.
1 1. The joint assembly, bicycle frame assembly, or vehicle subassembly of any of claims 1 to 10, wherein the at least one shaft comprises a first shaft and a second shaft.
12. The joint assembly, bicycle frame assembly, or vehicle subassembly of any of claims 1 to 1 1 wherein the shaft comprises a connecting component connecting the first shaft to the second shaft.
13. The joint assembly, bicycle frame assembly, or vehicle subassembly f claim 12, wherein the connecting component extends through each of the first and second shafts and is adapted to provide a biasing force to fix the axial position of the first and second shafts relative to the first and second housings respectively.
14. The joint assembly, bicycle frame assembly, or vehicle subassembly of any of claims 1 to 3, wherein the tapered surface of the inner diameter portion of the at least one housing has an angle a relative to an axis of the housing, wherein 1 °< a < 89°.
15. The joint assembly, bicycle frame assembly, or vehicle subassembly of any of claims 1 to 14, further comprising at least one spring element to provide a biasing force such that the shaft is biased against the housing.
EP18721704.7A 2017-04-21 2018-04-17 Adjustable joint assembly Active EP3612440B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201762488400P 2017-04-21 2017-04-21
PCT/EP2018/059755 WO2018192915A1 (en) 2017-04-21 2018-04-17 Adjustable joint assembly

Publications (2)

Publication Number Publication Date
EP3612440A1 true EP3612440A1 (en) 2020-02-26
EP3612440B1 EP3612440B1 (en) 2023-08-23

Family

ID=62104234

Family Applications (1)

Application Number Title Priority Date Filing Date
EP18721704.7A Active EP3612440B1 (en) 2017-04-21 2018-04-17 Adjustable joint assembly

Country Status (6)

Country Link
US (1) US11841047B2 (en)
EP (1) EP3612440B1 (en)
JP (3) JP2020517506A (en)
CN (1) CN110869270B (en)
ES (1) ES2963069T3 (en)
WO (1) WO2018192915A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110869270B (en) 2017-04-21 2022-10-21 圣戈班性能塑料万科有限公司 Adjustable joint assembly
TWI764109B (en) 2019-03-22 2022-05-11 美商聖高拜塑膠製品公司 Composite bearing and method of making and using the same

Family Cites Families (49)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US130945A (en) * 1872-08-27 Improvement in thill-couplings
US353330A (en) * 1886-11-30 Roller-bearing for velocipedes
US1374267A (en) * 1920-04-28 1921-04-12 George R Whitehead Diamond-polishing machine
CH106595A (en) * 1923-10-30 1924-09-01 Aegler A G Uhrenfabrik Rolex Shaft bearing.
CH131294A (en) * 1928-03-19 1929-01-31 Koeln Lindenthaler Metallwerke Vibration damping device for vehicles.
US1891405A (en) * 1930-03-21 1932-12-20 Standard Process Corp Cylinder mounting for printing presses
US1957781A (en) 1933-08-10 1934-05-08 Thompson Prod Inc Joint
NL72155C (en) 1948-11-13 1953-04-15
US2913251A (en) * 1958-02-17 1959-11-17 Thompson Ramo Wooldridge Inc Self-adjusting pivot bushing for vehicle suspension
US3182986A (en) * 1963-09-04 1965-05-11 Arthur C Brockman Resilient bushing structure
FR1593221A (en) 1967-11-06 1970-05-25
US3876231A (en) * 1973-01-18 1975-04-08 Anthony Geisel Sectional velocipede
US4101227A (en) * 1977-01-06 1978-07-18 Trw Inc. Pivot joint
US4191488A (en) * 1977-05-23 1980-03-04 Harry Bickerton Limited Securement arrangement for bicycle bearing assembly
JPS6347596Y2 (en) 1980-12-08 1988-12-08
DE3711971A1 (en) 1987-04-09 1988-10-27 Lemfoerder Metallwaren Ag SELF-ADJUSTING PIVOT JOINT WITH AXIAL GAME FOR MOTOR VEHICLES
US5217241A (en) * 1990-09-18 1993-06-08 Ocean State International Inc. Bicycle suspension system
US5024121A (en) * 1990-10-15 1991-06-18 Hsieh Kin H Hub assembly of a bicycle and the like
US5230142A (en) 1992-03-20 1993-07-27 Cooper Power Systems, Inc. Operating and torque tool
FR2691220B1 (en) * 1992-05-14 1995-09-08 Lavallard Christian DEVICE FOR ALLOWING CHANGE IN THE LINING OF A BEARING WITHOUT INTERRUPTING ITS OPERATION.
CN2195502Y (en) 1993-12-06 1995-04-26 罗士中 Real rocker arm single-tube suspensing stand for bicycle
DE59402543D1 (en) 1994-09-21 1997-05-28 Sen Heinrich Menze Resilient stem
FR2726532A1 (en) 1994-11-04 1996-05-10 Toulet Claude Device for transformation of bicycle crank lever oscillations into continuous rotational movement
US5681135A (en) 1995-01-19 1997-10-28 Simonson; Peter Melott Threaded fastener with multi-stage torque limiting applicator
DE19503047A1 (en) * 1995-02-01 1996-08-08 Gnieser Gmbh Auto Technik Front wheel suspension for motorcycles
DE19513764A1 (en) 1995-04-11 1996-10-17 Thomas Ripa Quick-change axle for bicycle wheel bearings
US5571184A (en) 1995-06-07 1996-11-05 Wright Medical Technology, Inc. Graft fixation device and method of using
DE19629559B4 (en) 1996-07-22 2007-08-02 Markus Storck bicycle frame
US5927741A (en) * 1998-12-15 1999-07-27 Chi; Yi-Chen Cushion device for a bicycle
DE29904311U1 (en) 1999-03-09 1999-07-08 Chi Damping device for a bicycle
DE10135622A1 (en) * 2001-07-21 2003-02-06 Bayerische Motoren Werke Ag Child's bicycle has extension element connected to forward end section of main frame tube and axially adjustable, and steering column is fastened at forward end of extension element
US7033294B2 (en) 2003-06-11 2006-04-25 Specialized Bicycle Components Bicycle rear derailleur guard
JP4323887B2 (en) 2003-07-16 2009-09-02 株式会社ムラコシ精工 Roller device
CN2767305Y (en) 2004-11-08 2006-03-29 重庆宗申技术开发研究有限公司 Motorbicycle engine suspended mounting arrangement
WO2007133681A2 (en) 2006-05-11 2007-11-22 Fallbrook Technologies Inc. Continuously variable drivetrain
US7717212B2 (en) 2006-08-25 2010-05-18 Split Pivot, Inc. Vehicle suspension systems for seperated acceleration responses
DE102007010790A1 (en) 2007-03-02 2008-09-11 Continental Aktiengesellschaft Air spring and damping unit for undercarriages of vehicles, particularly for bikes motor bikes, has cylinder hookup articulation point on vehicle frame or on car body and with another articulation point on undercarriage
DE102008027413A1 (en) 2008-06-09 2010-03-18 Tien Hsin Industries Co., Ltd., Ta-Li Bush for bicycle headset, has self lubricating layer made of specific material provided at peripheral side of ring
DE102009012765A1 (en) 2009-03-12 2010-09-16 Jochen Klieber Frame element of a spring-loaded bicycle frame for guiding a pipe
DE102009013339A1 (en) 2009-03-16 2010-09-23 Jochen Klieber Device for guiding a chain
DE112010003321T5 (en) 2009-08-19 2012-08-16 Rocky Mountain Bicycles, A Division Of Procycle Group Inc. Swivel joint for bicycle frame suspension
WO2011048186A1 (en) 2009-10-21 2011-04-28 Zero-Max Holding Dk A/S Torque limiting assembly
JP5649740B2 (en) * 2010-11-19 2015-01-07 サン−ゴバン パフォーマンス プラスティックス コーポレイション Bushing, composite, and method of forming a bushing
EP2863076B1 (en) * 2012-06-19 2021-02-24 Fuji Electric Co., Ltd. Composite sliding bearing and wind-powered electricity generation device using this bearing
CN102758860B (en) * 2012-07-27 2015-04-15 重庆大易用机械有限公司 Conical-surface friction type overrunning clutch
CN103352924A (en) 2013-07-22 2013-10-16 浙江上风实业股份有限公司 Heavy-load hub cone interference fitting structure and installing and dismantling method thereof
DE102013214582B4 (en) 2013-07-25 2024-03-07 Bayerische Motoren Werke Aktiengesellschaft Combined pivot bearing and front suspension for a motorcycle
CH708697B1 (en) 2013-10-11 2017-09-15 Flow Ag Two-wheeler with a rear suspension.
CN110869270B (en) 2017-04-21 2022-10-21 圣戈班性能塑料万科有限公司 Adjustable joint assembly

Also Published As

Publication number Publication date
US11841047B2 (en) 2023-12-12
CN110869270B (en) 2022-10-21
JP2023175844A (en) 2023-12-12
EP3612440B1 (en) 2023-08-23
CN110869270A (en) 2020-03-06
WO2018192915A1 (en) 2018-10-25
US20180306238A1 (en) 2018-10-25
JP2022023905A (en) 2022-02-08
ES2963069T3 (en) 2024-03-25
JP2020517506A (en) 2020-06-18

Similar Documents

Publication Publication Date Title
EP3865739B1 (en) Rotary shaft seal
JP2023175844A (en) adjustable joint assembly
US10507751B2 (en) Bearing for use in seat back assemblies
CN110612411A (en) Seal, assembly and method of use
US10926789B2 (en) Steering assembly
JP2023156341A (en) torque control system
CN111629952B (en) Steering assembly
US20200232508A1 (en) Assembly for a bearing and methods of making and using the same
US20160288816A1 (en) Steering assembly
WO2021116435A1 (en) Assembly comprising a tolerance ring between two components with desired slipping torque at the surfaces of contact
US20230392652A1 (en) Friction pad, assembly, and method of making and using the same
KR102671532B1 (en) Strut bearings, assemblies, and methods of making and using the same
US20220128087A1 (en) Bearing for partially spherical component and method of making and using the same
US11448258B2 (en) Strut bearing, assembly, and method of making and using the same

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: UNKNOWN

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20190920

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

17Q First examination report despatched

Effective date: 20200923

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: EXAMINATION IS IN PROGRESS

RAP3 Party data changed (applicant data changed or rights of an application transferred)

Owner name: SAINT-GOBAIN PERFORMANCE PLASTICS RENCOL LIMITED

REG Reference to a national code

Ref country code: DE

Ref legal event code: R079

Ref document number: 602018055899

Country of ref document: DE

Free format text: PREVIOUS MAIN CLASS: B62K0019180000

Ipc: F16C0025020000

Ref legal event code: R079

Ipc: F16C0025020000

RIC1 Information provided on ipc code assigned before grant

Ipc: B62K 19/18 20060101AFI20221219BHEP

RIC1 Information provided on ipc code assigned before grant

Ipc: F16C 17/10 20060101ALI20230113BHEP

Ipc: B62K 19/18 20060101ALI20230113BHEP

Ipc: F16C 25/02 20060101AFI20230113BHEP

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20230316

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602018055899

Country of ref document: DE

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230822

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG9D

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20230823

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1602898

Country of ref document: AT

Kind code of ref document: T

Effective date: 20230823

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231124

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231223

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231226

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231123

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231223

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20231124

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2963069

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20240325

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20230823

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CZ

Payment date: 20240326

Year of fee payment: 7